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  • AERODYNAMICS  (2,983)
  • 42.75
  • 2010-2014  (49)
  • 1985-1989  (2,967)
  • 1950-1954  (16)
  • 1
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    Twee nieuwe tweestaarten in Nederland (Diplura) (2014)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.43 (2014) p.5
    Details
    Publication Date: 2017-03-16
    Description: Tweestaarten Diplura behoren met de springstaarten Collembola en beentasters Protura tot de Entognatha. Dat zijn kleine ongevleugelde bodemdieren met zes poten, die zich onderscheiden van de insecten door hun verzonken monddelen. Tot nu toe waren twee soorten voor Nederland gemeld, maar voor België 13. Tijdens een onderzoek naar in mierennesten levende organismen werden twee soorten gevonden die nog niet uit Nederland bekend waren. Verder onderzoek zal zeker nog meer nieuwe tweestaarten kunnen opleveren.
    Keywords: Diplura ; Nederland ; Campodea lubbocki ; Campodea plusiochaeta ; verspreiding ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
    Type: Article / Letter to the editor
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  • 2
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    De kriebelmuggen van Nederland en Vlaanderen (Diptera: Simuliidae) (2014)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.43 (2014) p.67
    Details
    Publication Date: 2017-03-16
    Description: Larven van kriebelmuggen komen uitsluitend voor in stromend water, waar ze met hun waaiervormige monddelen deeltjes filteren uit het voorbij stromende water. Het zijn goede indicatoren voor zuurstofrijk water. Tot nu toe was niet duidelijk welke soorten precies voorkomen in Nederland en België en de determinatie van kriebelmuggen wordt vaak als lastig beschouwd. Om dit te verhelpen, presenteren we hier determinatietabellen voor alle in Nederland en België voorkomende soorten, zowel voor larven van het laatste stadium als voor poppen.
    Keywords: Diptera ; Simuliidae ; Nederland ; België ; herkenning ; verspreiding ; ecologie ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
    Type: Article / Letter to the editor
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  • 3
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    Recente aanvullingen op de Nederlandse loopkevercatalogus (Coleoptera: Carabidae) (2014)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.43 (2014) p.17
    Details
    Publication Date: 2017-03-16
    Description: De catalogus van de Nederlandse kevers uit 2010 geeft het meest recente overzicht van de Nederlandse kevers. Er staan 372 soorten loopkevers op deze lijst. Per soort wordt een overzicht gegeven van de provincies waaruit waarnemingen bekend zijn. Voor elk zogenaamd provincierecord is een collectie-exemplaar aangeduid als bewijsexemplaar. Sinds 2010 is er veel nieuwe informatie over loopkevers bekend geworden. In dit artikel worden de wijzigingen in de lijst toegelicht.
    Keywords: Coleoptera ; Carabidae ; Nederland ; verspreiding ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
    Type: Article / Letter to the editor
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  • 4
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    De reuzenertswesp Leucospis dorsigera nieuw voor Nederland (Hymenoptera: Chalcidoidea) (2014)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.43 (2014) p.1
    Details
    Publication Date: 2017-03-16
    Description: Hoe een leek op het gebied van wespen en bijen toch een leuke vondst kan doen. Op zonnige dagen gaat de auteur regelmatig op ‘tuinsafari’. Een tuin waarin rekening wordt gehouden met vogels en insecten, door keuze van beplanting en het ophangen van insectenhotels. De inspanningen leverden op 23 juli 2014 een opvallende wesp op. In een bijna automatische reactie werden snel foto’s gemaakt, in de hoop ze later te kunnen determineren. De wesp vloog daarna weg en werd niet meer gezien. Na determinatie blijkt het reuzenertswesp Leucospis dorsigera te zijn, een nieuwe soort bronswesp voor Nederland.
    Keywords: Hymenoptera ; Chalcidoidea ; Leucospis dorsigera ; Nederland ; herkenning ; biologie ; verspreiding ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
    Type: Article / Letter to the editor
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  • 5
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    Twee nieuwe citroenzweefvliegen voor Nederland: Xanthogramma dives en X. stackelbergi (Diptera: Syrphidae) (2014)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.43 (2014) p.27
    Details
    Publication Date: 2017-03-16
    Description: De gewone citroenzweefvlieg Xanthogramma pedissequum is een eenvoudig te herkennen zweefvlieg. Tenminste, dat dachten we tot voor kort. Nu blijkt dat de bijna identieke X. dives en X. stackelbergi ook in Nederland rondvliegen. Gelukkig zijn er enkele kenmerken waarmee deze drie soorten citroenzweefvlieg in het veld redelijk herkenbaar blijken. In dit artikel bespreken we deze kenmerken en geven we informatie over verspreiding en vliegtijden van de drie soorten.
    Keywords: Diptera ; Syrphidae ; Xanthogramma dives ; Xanthogramma stackelbergi ; Nederland ; herkenning ; verspreiding ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
    Type: Article / Letter to the editor
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  • 6
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    Blaaskopvliegen van het genus Leopoldius in de Benelux (Diptera: Conopidae) (2014)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.43 (2014) p.55
    Details
    Publication Date: 2017-03-16
    Description: Wespblaaskoppen Leopoldius worden ondanks hun opvallende uiterlijk maar weinig waargenomen. De soorten zijn lastig van elkaar te onderscheiden en bovendien werden tot voor kort variabele kenmerken gebruikt, wat tot veel verwarring heeft geleid. Nu blijkt dat alleen vrouwtjes met zekerheid te herkennen zijn aan de vorm van het klampje. Dit is een lepelvormig uitsteeksel onder het vijfde achterlijfsegment. Het wordt gebruikt bij het afzetten van eieren op een gastheer. Waarschijnlijk zijn limonadewespen de belangrijkste gastheer van Leopoldius. In dit artikel wordt een nieuwe soort voor België en een nieuwe soort voor Luxemburg gemeld. Daarnaast wordt een overzicht geboden van waarnemingen in Nederland, België en Luxemburg en een sleutel tot de Noordwest-Europese soorten.
    Keywords: Diptera ; Conopidae ; Leopoldius ; Nederland ; België ; Luxemburg ; herkenning ; biologie ; verspreiding ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
    Type: Article / Letter to the editor
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  • 7
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    Eerste larvenvondst van de kokerjuffer Molanna albicans buiten Drenthe (Trichoptera: Molannidae) (2014)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.43 (2014) p.93
    Details
    Publication Date: 2017-03-16
    Description: Ondanks de fors toegenomen aandacht voor watermacrofauna sinds begin jaren 1980 is de schietmot Molanna albicans maar sporadisch aangetroffen. In dit artikel wordt de eerste larvenvondst van M. albicans buiten Drenthe beschreven. Samen met de vindplaatsen in Drenthe is de soort nu van vijf vennen in Nederland bekend. Aanvullend worden de determinatiekenmerken aan de hand van foto’s geïllustreerd.
    Keywords: Trichoptera ; Molannidae ; Molanna albicans ; Nederland ; verspreiding ; biologie ; herkenning ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
    Type: Article / Letter to the editor
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  • 8
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    Spatial and temporal distribution of caddisfly larvae in two lowland streams in The Netherlands (Trichoptera) (2014)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.42 (2014) p.81
    Details
    Publication Date: 2017-03-16
    Description: Caddisflies are a species rich insect order. The adults are moth-like, but their wings bear hairs instead of scales. The larvae are aquatic and live in self-constructed cases, made of plant material, sand or debris. The species are used as indicators of water quality, but much is still not known about their biology and ecology. In this paper the preferred substrates and phenology of the larvae of 13 species are described, using the data of a survey of two lowland streams in the east of the Netherlands.
    Keywords: Trichoptera ; ecology ; phenology ; Netherlands ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
    Type: Article / Letter to the editor
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  • 9
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    Slakkendodende vliegen van het genus Psacadina in Nederland en België (Diptera: Sciomyzidae) (2014)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.42 (2014) p.37
    Details
    Publication Date: 2017-03-16
    Description: Slakkendodende vliegen danken hun naam aan hun roofzuchtige, parasitaire larven, die het op slakken gemunt hebben. Uit België en Nederland zijn circa 60 soorten uit deze familie bekend, maar er zijn er zeker meer te ontdekken. Dit artikel meldt een nieuwe soort voor de Nederlandse fauna uit het genus Psacadina, dat in beide landen drie soorten telt. De herkenning en het voorkomen van de drie soorten wordt uitgebreid besproken.
    Keywords: Diptera ; Sciomyzidae ; Psacadina ; Nederland ; België ; biologie ; herkenning ; verspreiding ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
    Type: Article / Letter to the editor
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  • 10
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    De zwarte vlieg Bibio venosus nieuw voor de Nederlandse fauna (Diptera: Bibionidae) (2014)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.42 (2014) p.33
    Details
    Publication Date: 2017-03-16
    Description: Zwarte vliegen behoren tot de muggen, maar door hun korte antennen doen ze oppervlakkig aan vliegen denken. De mannetjes zien er met hun grote kop en grote ogen heel anders uit dan de vrouwtjes, die een kleine kop met kleine ogen hebben. In het voorjaar vormen sommige soorten opvallend grote zwermen op windluwe plekken. Aan de 17 soorten die reeds uit Nederland bekend waren, kan er nu één worden toegevoegd: Bibio venosus.
    Keywords: Diptera ; Bibionidae ; Bibio venosus ; herkenning ; biologie ; verspreiding ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
    Type: Article / Letter to the editor
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  • 11
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    Uitbreiding van de hooiwagen Astrobunus leavipes (Opiliones) (2014)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.42 (2014) p.11
    Details
    Publication Date: 2017-03-16
    Description: Astrobunus laevipes is een hooiwagen die via het Rijnbekken recentelijk ons land is binnengekomen. Er waren al vondsten langs de Waal en Nederrijn in Gelderland en het meest oostelijke puntje van de provincie Utrecht. Door gerichte inventarisaties kunnen wij de hooiwagen nu nieuw voor de provincies Zuid-Holland en Noord-Brabant melden. Daarnaast is er van A. laevipes nu ook een waarneming langs de IJssel en enkele westelijker in de provincie Utrecht. Allerlei rivierbegeleidende biotopen langs (uitlopers van) de Nederrijn en Waal worden al door deze opmerkelijke hooiwagen bevolkt, maar de noordelijke uitbreiding via de IJsselvallei lijkt veel trager te verlopen. De Maas lijkt nog niet bereikt.
    Keywords: Opiliones ; Astrobunus leavipes ; Nederland ; verspreiding ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
    Type: Article / Letter to the editor
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  • 12
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    Vierde aanvulling op de naamlijst van Nederlandse sluipvliegen (Diptera: Tachinidae) (2014)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.43 (2014) p.43
    Details
    Publication Date: 2017-03-16
    Description: De familie der sluipvliegen is één der soortenrijkste vliegenfamilies in ons land. De larven ontwikkelen zich inwendig in ongewervelden, veelal vlinderrupsen. De familie is in ons land relatief goed bestudeerd. In dit artikel wordt wederom een soort voor het eerst uit ons land vermeld. Hiermee komt het totaal aantal soorten dat in Nederland ooit vastgesteld is op 334.
    Keywords: Diptera ; Tachinidae ; Pexopsis aprica ; Nederland ; verspreiding ; biologie ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
    Type: Article / Letter to the editor
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  • 13
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    Bamboewormen in Nederland, met Micromaldane ornithochaeta nieuw voor Nederland (Polychaeta: Maldanidae) (2014)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.43 (2014) p.111
    Details
    Publication Date: 2017-03-16
    Description: Mariene borstelwormen vormen een ecologisch belangrijke, soortenrijke groep. Van diverse families is niet veel bekend over het voorkomen in Nederland en de bamboewormen (familie Maldanidae) behoren tot de slechtst bekende groepen. Bamboewormen danken hun naam aan de lange en aan het uiteinde verdikte segmenten. In dit artikel wordt een nieuwe bamboeworm voor Nederland besproken en een opsomming gegeven van de nu bekende inheemse soorten.
    Keywords: Polychaeta ; Maldanidae ; Micromaldane ornithochaeta ; Nederland ; herkenning ; verspreiding ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 14
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    Slakkendodende vliegen van het genus Anticheta in Nederland, met twee soorten nieuw voor de fauna (Diptera: Sciomyzidae) (2014)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.42 (2014) p.47
    Details
    Publication Date: 2017-03-16
    Description: Slakkendodende vliegen zijn nog relatief slecht onderzocht in ons land, zeker de kleine soorten. De vertegenwoordigers van het genus Anticheta zijn kleine vliegjes, waarvan slechts twee soorten uit ons land bekend waren. Uitgebreider onderzoek, zowel in collecties als in het veld, heeft twee nieuwe soorten voor de fauna aan het licht gebracht: Anticheta nigra en A. obliviosa. Van de eerste soort waren wereldwijd slechts acht exemplaren bekend.
    Keywords: Diptera ; Sciomyzidae ; Anticheta ; Nederland ; herkenning ; biologie ; verspreiding ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
    Type: Article / Letter to the editor
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  • 15
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    Het dotterbloemgitje Cheilosia frontalis nieuw voor Nederland (Diptera: Syrphidae) (2014)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.43 (2014) p.37
    Details
    Publication Date: 2017-03-16
    Description: Zelfs in een goed onderzochte insectengroep als de zweefvliegen zijn nog altijd nieuwe soorten voor de Nederlandse fauna te ontdekken. Ook in 2014 was het weer raak, dit keer in het fraaie natuurgebied rond de Drentsche Aa. Het lijkt niet toevallig dat deze aanvulling op de Nederlandse fauna juist hier werd gevonden. Deze vindplaats vult ecologische informatie uit het buitenland aan, waardoor langzamerhand een beeld begint te ontstaan van de levenswijze van deze zeldzame zweefvlieg, waarover tot voor kort weinig bekend was.
    Keywords: Diptera ; Syrphidae ; Cheilosia frontalis ; Nederland ; herkenning ; biologie ; verspreiding ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
    Type: Article / Letter to the editor
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  • 16
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    Nieuwe vondsten van de doornkaakzandbij Andrena trimmerana in Nederland (Hymenoptera: Apoidea: Andrenidae) (2014)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.42 (2014) p.75
    Details
    Publication Date: 2017-03-16
    Description: De doornkaakzandbij ziet er in het voorjaar een beetje anders uit dan in de zomer. Daarom worden de voorjaarsdieren door sommigen tot een andere soort beschouwd dan de zomerdieren. Uit Nederland zijn slechts drie exemplaren bekend: twee uit het voorjaar en één uit de zomer. Toevallig komen alle exemplaren uit hetzelfde gebied. Of is dit geen toeval?
    Keywords: Hymenoptera ; Apoidea ; Andrenidae ; Andrena trimmerana ; Nederland ; herkenning ; verspreiding ; biologie ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
    Type: Article / Letter to the editor
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  • 17
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    Het Sachalin-elfje Melangyna pavlovskyi nieuw voor Nederland (Diptera: Syrphidae) (2014)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.42 (2014) p.29
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    Publication Date: 2017-03-16
    Description: Elfjes behoren tot de vroegste zweefvliegen die in het voorjaar uit de pop kruipen. Rond bloeiende wilgen wemelt het vaak van wilgenelfjes Melangyna lasiophthalma, waardoor het zoeken naar de zeldzamere soorten soms lastig is. Toch zijn de meeste soorten relatief makkelijk van elkaar te onderscheiden. Met de vondst van het Sachalinelfje M. pavlovskyi wordt het echter weer iets lastiger.
    Keywords: Diptera ; Syrphidae ; Melangyna pavlovskyi ; Nederland ; herkenning ; verspreiding ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 18
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    Drie steltmuggen nieuw voor Nederland (Diptera: Limoniidae) (2014)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.42 (2014) p.19
    Details
    Publication Date: 2017-03-16
    Description: Steltmuggen lijken op langpootmuggen en zijn daar nauw aan verwant. Veel soorten zijn groot en karakteristiek gekleurd, maar toch zijn ze in Nederland nog weinig bestudeerd. Dit artikel bewijst dat er nog veel te ontdekken valt: in één jaar tijd zijn drie soorten gevonden die nog niet uit ons land bekend waren: Atypophthalmus inustus, Molophilus niger en Arctoconopa melampodia. Hiermee komt het totaal aantal soorten voor Nederland op 149. De nieuwe meldingen sluiten goed aan op het bekende verspreidingsgebied.
    Keywords: Diptera ; Limoniidae ; Nederland ; verspreiding ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 19
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    De wants Jalla dumosa na 45 jaar weer in Nederland waargenomen (Heteroptera: Pentatomidae) (2014)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.43 (2014) p.9
    Details
    Publication Date: 2017-03-16
    Description: Jalla dumosa is een in Nederland zeer zeldzame pentatomide, die in 1969 voor het laatst was waargenomen op Terschelling. Na 45 jaren zonder waarnemingen werd ze in 2014 weer in klein aantal waargenomen in de Kooiduinen op Ameland. Rupsen van onder andere de duinparelmoervlinder en de sint-jansvlinder stonden daar op het menu. In deze bijdrage wordt informatie samengevat over de vondsten in Nederland, de biologie en de verspreiding van de soort.
    Keywords: Heteroptera ; Pentatomidae ; Jalla dumosa ; Nederland ; verspreiding ; biologie ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 20
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    The exotic jellyfish Blackfordia virginica introduced into the Netherlands (Cnidaria: Hydrozoa) (2014)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.43 (2014) p.103
    Details
    Publication Date: 2017-03-16
    Description: In August 2014 the exotic jellyfish Blackfordia virginica was captured in the harbour of Amsterdam. This is the first confirmed record of this species in the Netherlands, although in October 2013 a possible specimen was filmed and released. This indicates that the species might be established in the Amsterdam area, although repeated introduction with ballast water cannot be ruled out. In September 2014 hydrozoan polyp colonies closely resembling those of B. virginica were collected near IJmuiden in the Noordzeekanaal, a canal connecting Amsterdam with the North Sea at IJmuiden.
    Keywords: Cnidaria ; Hydrozoa ; Blackfordia virginica ; Netherlands ; exotic species ; distribution ; identification ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 21
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    Het hooiwagengenus Trogulus in Nederland (Opiliones: Trogulidae) (2014)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.42 (2014) p.1
    Details
    Publication Date: 2017-03-16
    Description: Wie een steen of boomstronk omkeert en voor het eerst een Trogulus opmerkt, zal dit bizarre beest niet direct associëren met een hooiwagen. Met de korte, stevige poten, het afgeplatte achterlijf dat overdekt is met strooisel en zand, en een trage manier van voortbewegen is het een ongewone verschijning. De soorten van dit geslacht zijn bodembewoners die zich voornamelijk voeden met kleine huisjesslakken. Uit ons land waren tot nu toe twee soorten bekend. De identiteit van een van die twee was lang onzeker, maar door nieuwe inzichten is nu duidelijk om welke soort het werkelijk gaat. In Nederland blijkt bovendien nog een derde soort voor te komen, die hier voor het eerst gemeld wordt.
    Keywords: Opiliones ; Trogulidae ; Trogulus ; Nederland ; herkenning ; verspreiding ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 22
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    De gouden stamjager Choerades igneus nieuw voor Nederland (Diptera: Asilidae) (2014)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.43 (2014) p.47
    Details
    Publication Date: 2017-03-16
    Description: Roofvliegen zijn met 40 Nederlandse soorten een vrij kleine groep, die behoorlijk goed is onderzocht. Het gebeurt dan ook niet vaak dat er een nieuwe soort voor de Nederlandse fauna kan worden opgetekend. De meeste roofvliegen zijn grijze vliegen, zo niet de stamjagers van het genus Choerades. Dit zijn juist vrij opvallend gekleurde vliegen. Zo heeft de rode dennenstamjager Choerades gilvus een rood gekleurd achterlijf. Opmerkelijk genoeg blijkt dat in Nederland juist onder deze opvallende verschijning twee soorten schuilgaan.
    Keywords: Diptera ; Asilidae ; Choerades igneus ; Nederland ; verspreiding ; biologie ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 23
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    Bruchus brachialis, een zaadkever nieuw voor de Nederlandse fauna (Coleoptera: Chrysomelidae) (2014)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.43 (2014) p.23
    Details
    Publication Date: 2017-03-16
    Description: Onlangs werd op een braakliggend terrein in Roermond de zaadkever Bruchus brachialis verzameld. Dit is de eerste Nederlandse vondst van deze zuidelijke soort. Een reeks recente waarnemingen uit de ons omringende landen laat zien dat deze soort al enige jaren in een noordwaartse areaaluitbreiding verwikkeld is. Met deze ontdekking komt het aantal Nederlandse Bruchus-soorten op zeven.
    Keywords: Coleoptera ; Chrysomelidae ; Nederland ; herkenning ; biologie ; verspreiding ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 24
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    De springstaart Entomobrya unostrigata nieuw voor noordwest Europa (Hexapoda: Collembola: Entomobryidae) (2014)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.42 (2014) p.63
    Details
    Publication Date: 2017-03-16
    Description: Nieuw gevormd landschap, zoals jonge duinvalleien, opgespoten polders en bedrijventerreinen in ontwikkeling vormen de habitat van gespecialiseerde soorten. Je moet tegen een stootje kunnen om in een dergelijke zandige, schaars begroeide omgeving te overleven. Vooral langdurig warme, droge perioden vormen een probleem voor vochtminnende bodemdieren. De springstaartsoorten die hier overleven zijn warmteminnend en droogteresistent, een bijzondere combinatie voor bodemdieren. Dit geldt ook voor Entomobrya unostrigata, een nieuwe aanwinst voor de fauna van Noordwest-Europa. Er is een aantal populaties van deze soort op de Tweede Maasvlakte gevonden. De dieren zaten hier onder stenen en hout op opgespoten zand.
    Keywords: Collembola ; Entomobryidae ; Entomobrya unostrigata ; Nederland ; herkenning ; verspreiding ; biologie ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 25
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    Sigalionide zeerupsen in Nederland, met Fimbriosthenelais minor nieuw voor Nederland (Polychaeta: Sigalionidae) (2014)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.42 (2014) p.71
    Details
    Publication Date: 2017-03-16
    Description: De Polychaeta vormen een groep van vrijwel uitsluitend mariene wormen, gekenmerkt door een geleed lichaam met aan de meeste leden een tamelijk groot aantal borstels. Het is een soortenrijke groep; ze spelen een belangrijke rol in de ecologie en diversiteit van vooral zachte, maar ook harde zeebodems. In vergelijking met de kreeftachtigen en weekdieren, eveneens soortenrijke groepen in dezelfde biotoop, zijn borstelwormen minder goed onderzocht. In dit artikel wordt de zeerups Fimbriosthenelais minor nieuw voor ons land gemeld. Met name op stenige en schelprijke bodems zijn nog meer nieuwe borstelwormen voor ons land te verwachten.
    Keywords: Polychaeta ; Sigalionidae ; Fimbriosthenelais minor ; Nederland ; herkenning ; verspreiding ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 26
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    Verspreiding en biotoop van het kalkdoorntje Tetrix tenuicornis in de Gelderse Poort (Orthoptera) (2014)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.42 (2014) p.55
    Details
    Publication Date: 2017-03-16
    Description: Het kalkdoorntje is een zeldzame sprinkhanensoort, die vooral bekend is uit Zuid-Limburg en van enkele locaties in het rivierengebied. Over het voorkomen van dit kleine sprinkhaantje binnen de Gelderse Poort was lange tijd weinig bekend. Pas vanaf 2007 worden regelmatig waarnemingen gedaan. Toevallige waarnemingen op, voor de auteur, onverwachte locaties vormden de aanleiding voor een grondige inventarisatie in de jaren 2011-2013. Hieruit komt naar voren dat het kalkdoorntje een ruime verspreiding heeft binnen de Gelderse Poort en een meer diverse biotoopkeuze heeft dan voorheen bekend was.
    Keywords: Orthoptera ; Tetrigidae ; Tetrix tenuicornis ; verspreiding ; biologie ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 27
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    Sensitivities of marine macrozoobenthos to environmental pressures in the Netherlands (2013)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.41 (2013) p.79
    Details
    Publication Date: 2015-12-09
    Description: The relative sensitivities of 309 common invertebrate species in Dutch marine waters are presented for environmental and anthropogenic pressures like organic enrichment, sedimentation and fisheries. The species were furthermore appointed to trophic groups like suspension and deposit feeders. The Dutch Ministry of Infrastructure and the Environment uses these data when calculating the Benthic Ecosystem Quality Index 2 and the Infaunal Trophic Index. These metrics aid in the mandatory monitoring of ecological quality for example for the European Water Framework Directive. The common Dutch species were selected based on their abundance according to, 1. the mwtl dataset including results of on-going monitoring programs issued by the Ministry, 2. the monitoring by volunteer scuba-divers for the anemoon Foundation and 3. the monitoring of fouling plates for the project setl.
    Keywords: macrozoobenthos ; marine ; Netherlands ; environment ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 28
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    De zeepissebed Uromunna spec, de eerste waarneming van de familie Munnidae in Nederland (Isopoda) (2013)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.41 (2013) p.43
    Details
    Publication Date: 2015-12-09
    Description: Onze fauna verandert en de mariene fauna is daarop geen uitzondering. Zuidelijke soorten koloniseren onze kustwateren en exotische soorten worden door de mens aangevoerd. Voor sommige soorten is niet duidelijk waarom ze hier opduiken. De sterk veranderende kustbiotopen spelen ongetwijfeld eveneens een rol. Een niet-aflatende stroom onverwachte soorten, soms zelfs behorend tot nieuwe genera en zelfs families maken faunistisch onderzoek in de kustwateren verrassend en boeiend. In het kader van een inventarisatie van kreeftachtigen in het Deltagebied werden in de Oosterschelde bij Zierikzee verscheidene kleine monsters genomen van diverse substraten. De monsters van roodwieren bevatten een aantal opmerkelijke soorten. Dit artikel behandelt Uromunna spec., een zeepissebeddensoort van een familie die in ons land nog niet was aangetroffen.
    Keywords: Isopoda ; Munnidae ; Nederland ; Uromunna ; verspreiding ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 29
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    First record of a settled stomatopod Platysquilla eusebia in the North Sea (Malacostraca: Stomatopoda) (2013)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.41 (2013) p.31
    Details
    Publication Date: 2015-12-09
    Description: This paper describes the discovery of a settled juvenile specimen of the stomatopod Platysquilla eusebia on the Dutch part of the Dogger Bank in the central North Sea. This is the northernmost record in Europe. The species is native to the Mediterranean and to the Atlantic coast from Portugal up to France. Further investigations have to show if the species already forms populations this far north. As the planktonic stages of P. eusebia have already been recorded in prior years, the establishment of the species should not be a problem, providing the circumstances are favourable.
    Keywords: Malacostraca ; Stomatopoda ; Platysquilla eusebia ; distribution ; Netherlands ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 30
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    De springstaart Fasciosminthurus quinquefasciatus nieuw voor de Nederlandse fauna (Collembola: Bourletiellidae) (2013)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.40 (2013) p.1
    Details
    Publication Date: 2015-12-09
    Description: Met enige regelmaat duiken nieuwe springstaartsoorten op in ons land. Het vinden van een nieuwe soort is soms op toeval gebaseerd. Op een foto van een sprinkhaan was naast de linker voorpoot een klein, donker vlekje te zien. Uitvergroot bleek het om een klein springstaartje te gaan. Het zwart-wit gestreepte patroon liet geen ruimte voor twijfel over de determinatie: Fasciosminthurus quinquefasciatus, een nieuwe springstaart voor de Nederlandse fauna. In dit artikel wordt het genus en de soort voorgesteld, beschrijven we de habitat en geven we informatie over de verspreiding in de rest van Europa.
    Keywords: Collembola ; Bourletiellidae ; Fasciosminthurus quinquefasciatus ; Nederland ; verspreiding ; herkenning ; biologie ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 31
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    Duistere heiderouwzwever Exoprosopa cleomene duikt op in Nederlandse wolzwevercollectie (Diptera: Bombyliidae) (2013)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.39 (2013) p.49
    Details
    Publication Date: 2015-12-09
    Description: De roodbruine heiderouwzwever Exoprosopa capucina is een fraaie en karakteristieke koffiebruine verschijning op de Nederlandse heideterreinen. Zoals veel wolzwevers is deze te herkennen aan de vleugeltekening en de kleur van de lichaamsbeharing. Echter naarmate de dieren ouder worden verliezen ze deze beharing en wordt de determinatie lastiger. Vermoedelijk heeft het verfomfaaide uiterlijk van een vrouwtje Exoprosopa cleomene er voor gezorgd dat deze ruim 50 jaar onopgemerkt tussen de exemplaren van E. capucina heeft gestaan.
    Keywords: Diptera ; Bombyliidae ; Exoprosopa cleomene ; Nederland ; verspreiding ; herkenning ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 32
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    Sulcacis bidentulus, een nieuwe houtzwamkever voor de Nederlandse fauna (Coleoptera: Ciidae) (2013)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.39 (2013) p.7
    Details
    Publication Date: 2015-12-09
    Description: In de afgelopen jaren werd op verschillende plekken in Nederland een houtzwamkever gevonden die tot nu toe niet officieel gemeld werd: Sulcacis bidentulus. Deze soort valt binnen de zeer eenvormige familie Ciidae op door de kleur van de dekschilden, die duidelijk iets lichter bruin zijn dan de rest van het lichaam. De soort zou zich ontwikkelen in de bleke borstelkurkzwam, die voornamelijk op populieren groeit. Oudere vondsten ontbreken en de ontdekking van deze soort op meerdere locaties duidt op een recente vestiging in ons land. Dit sluit aan bij de geconstateerde uitbreiding in Midden-Europa.
    Keywords: Coleoptera ; Ciidae ; Sulcacis bidentulus ; Nederland ; verspreiding ; biologie ; herkenning ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 33
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    Vestiging van de boomkrekel Oecanthus pellucens in het rivierengebied (Orthoptera) (2013)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.39 (2013) p.35
    Details
    Publication Date: 2015-12-09
    Description: De boomkrekel is een slanke geelbruine krekel, die vooral opvalt door zijn melodieuze zang. Vroeger moest je naar Frankrijk om dit geluid te horen, maar tegenwoordig heerst ook in het rivierengebied bij Nijmegen een mediterrane sfeer. De boomkrekel is in 2004 voor het eerst langs de Waal gevonden en heeft zich daarna uitgebreid. In 2010 en 2011 heeft de Flora- en faunawerkgroep Gelderse Poort met vele vrijwilligers onderzoek gedaan naar de precieze verspreiding. In totaal werd de boomkrekel in 57 kilometerhokken gevonden en de verwachting is dat de soort zich de komende jaren verder zal uitbreiden.
    Keywords: Orthoptera ; Oecanthus pellucens ; Nederland ; verspreiding ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 34
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    De Nederlandse hongerwespen (Hymenoptera: Evanioidea: Gasteruptiidae) (2013)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.39 (2013) p.55
    Details
    Publication Date: 2015-12-09
    Description: Hongerwespen behoren tot de grote groep van de sluipwespen. Het zijn slanke wespjes die typisch met hangende pootjes vliegen, waarbij de verbrede achterschenen opvallen. Ze parasiteren bijen en mogelijk ook bepaalde angeldragende wespen en worden daarom vaak bij bijenhotels waargenomen. In het kader van dit artikel zijn de meldingen van Nederlandse hongerwespen kritisch beschouwd. In totaal zijn nu negen soorten uit ons land bekend, waarvan er hier maar liefst zes voor het eerst worden gemeld.
    Keywords: Hymenoptera ; Evanioidea ; Gasteruptiidae ; Nederland ; verspreiding ; herkenning ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 35
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    Marine fauna of hard substrata of the Cleaver bank and Dogger bank (2013)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.41 (2013) p.69
    Details
    Publication Date: 2015-12-09
    Description: As most of the sea bottom in the Dutch part of the North Sea consists of sand, marine fauna that live in association with hard substrates are rarely monitored. We report here on the results of a species inventory in June 2011 done by scuba-diving while focusing on a wreck on the Dogger Bank and on rocky bottoms on the Cleaver Bank. This resulted in various new records of species for the Dutch part of the North Sea. This result appeared for a large part linked to the added value of monitoring with scuba-divers. It is therefore concluded that scuba-divers should be used in addition to the more traditional monitoring methods in which dredges and grabs are used, if one aims at getting an accurate view of the biodiversity present in marine regions like the North Sea.
    Keywords: biodiversity ; hard substrata ; Netherlands ; marine ; scuba-diving ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 36
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    Benthic communities on hard substrates within the first Dutch offshore wind farm (OWEZ) (2013)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.41 (2013) p.59
    Details
    Publication Date: 2015-12-09
    Description: Five years after the commissioning of the offshore wind farm Egmond aan Zee, the monopiles and the rocks of the scour protection layers were covered by a wide variety of marine organisms. This paper describes the results of qualitative and quantitative assessments carried out in 2008 and 2011. The assessments were based on video footage, pictures and samples collected by divers at three different wind turbines. The ecological relevance of identified taxa is also discussed.
    Keywords: offshore wind farms ; Netherlands ; biodiversity ; benthic zone ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 37
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    De gouden kegelbij Coelioxys aurolimbata teruggevonden in het rivierengebied (Hymenoptera: Apoidea: Megachilidae) (2013)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.40 (2013) p.39
    Details
    Publication Date: 2015-12-09
    Description: De gouden kegelbij Coelioxys aurolimbata is uit ons land recent alleen bekend uit de zuidelijke helft van Limburg. Vóór 1960 kwam deze parasiet van de lathyrusbij Chalicodoma ericetorum ook in het rivierengebied voor. In juli van dit jaar werd de gouden kegelbij gevangen in Duiven. Mogelijk is dit de voorbode van een herovering van het rivierengebied door deze bedreigde soort.
    Keywords: Hymenoptera ; Apoidea ; Megachilidae ; Nederland ; Coelioxys aurolimbata ; verspreiding ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 38
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    The juwel anemone Corynactis viridis, a new order for the Netherlands (Cnidaria: Corallimorpharia) (2013)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.41 (2013) p.35
    Details
    Publication Date: 2015-12-09
    Description: During an expedition with scuba-divers to the Dutch part of the Brown Ridge in the central North Sea in June 2013, two colonies of the jewel anemone Corynactis viridis were found on the wreck Anna Graebe. With the jewel anemone both a new species and a new animal order, the Corallimorpharia, are added to the autochthonous fauna of the Netherlands. This species typically occurs in the Mediterranean and along the Atlantic coast from Portugal and the west British Isles up to Shetland. As other records of settled colonies of C. viridis in the North Sea were recently reported from Belgian, German and English waters, it is concluded that the jewel anemone, which used to be known as an occasional visitor, should now be considered autochthonous in the North Sea.
    Keywords: Cnidaria ; Corallimorpharia ; Netherlands ; Corynactis viridis ; distribution ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 39
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    De molkreeften Upogebia deltaura en U. stellata en geassocieerde soorten in de Noordzee (Decapoda: Upogebiidae) (2013)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.41 (2013) p.15
    Details
    Publication Date: 2015-12-09
    Description: In de bodem van de Noordzee leeft een bijzondere groep van kreeften. Zij brengen hun leven door in een ondergronds gangenstelsel: de molkreeften. Het zijn algemene bewoners van het Friese Front, de Oestergronden en de Klaverbank. In, op en bij deze kreeften leven verschillende andere diersoorten: parasitaire pissebedden, een mosdiertje en twee soorten tweekleppigen. Deze bijdrage gaat in op de ecologie van de molkreeften en hun symbionten.
    Keywords: Decapoda ; Upogebiidae ; Upogebia ; Nederland ; biology ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 40
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    Moss animals of the Dutch part of the North Sea and coastal waters of the Netherlands (Bryozoa) (2013)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.41 (2013) p.1
    Details
    Publication Date: 2015-12-09
    Description: Bryozoa or moss animals constitute a conspicuous and species-rich component of hardsubstrate benthic communities in marine and estuarine habitats. To gain insight into the biodiversity of these habitats, knowledge of bryozoan species is indispensable. Since the last comprehensive publication on Dutch species in 2004 much new information has become available. Particularly from the Dutch part of the Continental Flat of the North Sea, the largest natural area of the Netherlands, many new records have been collected. Other reasons to present an updated review are changes in nomenclature, the arrival of some exotic species and identification issues.
    Keywords: Bryozoa ; Netherlands ; checklist ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 41
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    Tephrochlaena oraria, een nieuwe afvalvlieg voor de Nederlandse fauna (Diptera: Heleomyzidae) (2013)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.40 (2013) p.35
    Details
    Publication Date: 2015-12-09
    Description: Heleomyzidae zijn kleine tot middelgrote vliegen. Ze krijgen niet veel aandacht, omdat de meeste soorten een nogal verborgen leven leiden en bovendien niet opvallend gekleurd of getekend zijn. De Nederlandse familienaam, afvalvliegen, is voor de meeste soorten niet echt passend, maar veel soorten van de subfamilie Heteromyzinae, waartoe Tephrochlaena oraria behoort, worden dan wel weer vaker rond afval aangetroffen. Tephrochlaena oraria is echter in meerdere opzichten een buitenbeentje. Met deze soort komt de lijst van Nederlandse Heleomyzidae op 49.
    Keywords: Diptera ; Heleomyzidae ; Tephrochlaena oraria ; Nederland ; verspreiding ; herkenning ; biologie ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 42
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    Komt de vermiljoenkever Cucujus cinnaberinus in azijnzuurvallen (Coleoptera: Cucujidae)? (2013)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.40 (2013) p.9
    Details
    Publication Date: 2015-12-09
    Description: Cucujus cinnaberinus is een recent voor Nederland ontdekte soort. De kever staat op de Habitatrichtlijn, wat onder meer betekent dat hij beschermd is en dat de populatie gemonitord dient te worden. Inventarisatie en monitoring gebeurt in het algemeen door het weghalen van schors van recent gestorven bomen. Hierdoor wordt het leefgebied van de kever echter flink aangetast. Wij voerden een klein onderzoek uit naar de mogelijkheden om C. cinnaberinus te vangen in azijnzuurvallen, zodat de habitat intact gelaten kan worden en de soort toch geïnventariseerd kan worden. Tijdens het voorjaar van 2013 werden vier vallen opgehangen op een locatie waar zich een populatie van deze soort bevindt. Er werden slechts twee individuen verzameld; de vangmethode lijkt dus niet bijzonder geschikt.
    Keywords: Coleoptera ; Cucujidae ; Cucujus cinnaberinus ; methode ; inventarisatie ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 43
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    Northward dispersal of the tanaid Zeuxo holdichi to the Netherlands (Crustacea: Tanaidae) (2013)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.39 (2013) p.95
    Details
    Publication Date: 2015-12-09
    Description: The tanaid Zeuxo holdichi, described in 1990 from Arcachon Bay in southwest France, has since then been recorded from west Portugal to northern Brittany and southwest England. The species is recorded here from the Netherlands, a further northward expansion of the range. It is hypothesised that Z. holdichi may be non-native to Europe.
    Keywords: Crustacea ; Tanaidae ; Zeuxo holdichi ; Netherlands ; distribution ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 44
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    Ecological relevance of shipwrecks in the North Sea (2013)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.41 (2013) p.49
    Details
    Publication Date: 2015-12-09
    Description: This paper reports on observations made during wreck dive expeditions in 2010-2012, in order to investigate the ecological relevance of shipwrecks on the Dutch Continental Shelf (dcs). Shipwrecks are biodiversity hotspots. The number of species recorded on shipwrecks is similar to the number of species found in soft bottoms of the entire dcs. The soft substrates, however, represent a vastly larger habitat on the dcs than the shipwrecks. Amongst many other taxa, juvenile and large Atlantic cod, linear skeleton shrimp, goldsinny wrasses and leopard spotted gobies were found in the shipwreck habitats. The presence of these important species and their absence from many other habitats, illustrate that shipwrecks function as key habitats, nurseries, and refugia that are rare or absent anywhere else in the Netherlands.
    Keywords: shipwrecks ; Netherlands ; biodiversity ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
    Type: Article / Letter to the editor
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  • 45
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    De hottentottenvilla Villa hottentotta toch op de Nederlandse lijst (Diptera: Bombyliidae) (2013)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.40 (2013) p.23
    Details
    Publication Date: 2015-12-09
    Description: Wolzwevers zijn vliegen waarvan de larven parasitair leven bij andere insecten. Wolzwevers van het genus Villa veroorzaken vaak determinatieproblemen. Deze problemen lijken verleden tijd met recent gepubliceerde taxonomische inzichten. Eindelijk konden nu ook de Nederlandse exemplaren van dit genus op naam gebracht worden. Deze bleken te behoren tot vier soorten, waarvan er twee vermoedelijk reeds zijn verdwenen.
    Keywords: Diptera ; Bombyliidae ; Villa hottentotta ; Nederland ; verspreiding ; herkenning ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 46
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    De bijzondere levensloop van de sluipwesp Acrodactyla quadrisculpta op de schaduwstrekspin Tetragnatha montana (Hymenoptera: Ichneumonidae, Araneae: Tetragnathidae) (2013)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.39 (2013) p.1
    Details
    Publication Date: 2015-12-09
    Description: Sluipwespen van de groep van de Polysphinctini hebben een bijzondere levenswijze. Het vrouwtje van wesp legt een eitje op het achterlijf van een spin. Wanneer het eitje is uitgekomen brengt de larve haar hele leven op het achterlijf van de spin door. Ze maakt kleine wondjes in de huid en voedt zich met lichaamsvloeistof van de spin. Na verloop van tijd ontwikkelt de larve bulten op de rug, een teken dat ze bijna volgroeid is. Ze zuigt dan de spin leeg, de ‘grote slurp’ genaamd, en verpopt zich in het web. In dit artikel wordt de levenswijze van één van deze soorten, Acrodactyla quadrisculpta, voor het eerst beschreven en geïllustreerd.
    Keywords: Hymenoptera ; Ichneumonidae ; Araneae ; Tetragnathidae ; biologie ; Nederland ; Acrodactyla quadrisculpta ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 47
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    Galvormende bladwespen op wilg in Nederland (Hymenoptera: Tenthredinidae: Nematinae) (2013)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.39 (2013) p.15
    Details
    Publication Date: 2015-12-09
    Description: De bladwespgenera Phyllocolpa, Tubpontania, Pontania en Euura hebben gemeenschappelijk dat ze gallen vormen op wilg. Recentelijk is er veel vernieuwend taxonomisch werk verricht aan deze groepen. In dit artikel wordt de Nederlandse situatie samengevat. Uit oudere literatuur waren 18 soorten bekend en in het recent gepubliceerde gallenboek worden nog eens 11 soorten voor het eerst voor ons land vermeld. In dit artikel worden nog acht soorten aan de lijst toegevoegd en twee soorten worden van de lijst afgevoerd. In totaal zijn nu 35 soorten galvormende bladwespen van wilg uit Nederland bekend.
    Keywords: Hymenoptera ; Tenthredinidae ; Nematinae ; Nederland ; verspreiding ; herkenning ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 48
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    De rode snuitvlieg Rhingia rostrata terug in Nederland (Diptera: Syrphidae) (2013)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.40 (2013) p.15
    Details
    Publication Date: 2015-12-09
    Description: Snuitvliegen zijn rare snuiters onder de zweefvliegen. Ze hebben een verlengd gezicht en een lange tong. Hiermee kunnen ze foerageren op bloemen met diepliggende nectar, in tegenstelling tot de meeste andere zweefvliegen. Als genus zijn de vliegen makkelijk herkenbaar, maar de zeer zeldzame soorten tussen de zeer algemene gewone snuitvlieg uithalen was niet altijd even makkelijk. In dit artikel wordt de herontdekking van de rode snuitvlieg beschreven en een tabel gegeven voor de drie Noordwest-Europese soorten.
    Keywords: Diptera ; Syrphidae ; Rhingia rostrata ; Nederland ; verspreiding ; herkenning ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 49
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    Eerste waarneming van de schietmot Ecclisopteryx dalecarlica in Nederland en nieuwe vondsten in België (Trichoptera: Limnephilidae) (2013)
    In:  Nederlandse Faunistische Mededelingen (0169-2453) vol.39 (2013) p.89
    Details
    Publication Date: 2015-12-09
    Description: De larven van Trichoptera heten kokerjuffers en leven in het water. Veel soorten bouwen een kokertje van zand, takjes of ander materiaal, vandaar de Nederlandse naam. De volwassen dieren lijken wel wat op nachtvlinders en worden schietmotten genoemd. De laatste jaren heeft het onderzoek naar deze dieren een grote vlucht genomen. Enerzijds spelen ze een rol als indicator voor de waterkwaliteit. De larven worden dan ook veel verzameld tijdens macrofaunabemonsteringen door waterschappen. Anderzijds is er een groeiende groep entomologen die schietmotten bestudeert. In dit artikel wordt Ecclisopteryx dalecarlica voorgesteld, een nieuwe soort voor Nederland.
    Keywords: Trichoptera ; Limnephilidae ; Ecclisopteryx dalecarlica ; Nederland ; Belgie ; verspreiding ; herkenning ; 42.75
    Repository Name: National Museum of Natural History, Netherlands
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  • 50
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    Nonequilibrium hypersonic aerothermodynamics (1989)
    In:  Other Sources
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    Publication Date: 2011-08-19
    Description: Nonequilibrium phenomena in hypersonic flows are examined on the basis of theoretical models and selected experimental data, in an introduction intended for second-year graduate students of aerospace engineering. Chapters are devoted to the physical nature of gas atoms and molecules, transitions of internal states, the formulation of the master equation of aerothermodynamics, the conservation equations, chemical reactions in CFD, the behavior of air flows in nonequilibrium, experimental aspects of nonequilibrium flow, a review of experimental results, and gas-solid interaction. Diagrams, graphs, and tables of numerical data are provided.
    Keywords: AERODYNAMICS
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  • 51
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    Transonic region of high dynamic response encountered on an elastic supercritical wing (1989)
    In:  Other Sources
    Details
    Publication Date: 2011-08-19
    Keywords: AERODYNAMICS
    Type: Journal of Aircraft (ISSN 0021-8669); 26; 870-875
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  • 52
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    Transonic aeroelasticity of fighter wings with active control surfaces (1989)
    In:  Other Sources
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    Publication Date: 2011-08-19
    Keywords: AERODYNAMICS
    Type: Journal of Aircraft (ISSN 0021-8669); 26; 682-684
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  • 53
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    Hypersonic parabolized Navier-Stokes code validation on a sharp nose cone (1989)
    In:  Other Sources
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    Publication Date: 2011-08-19
    Keywords: AERODYNAMICS
    Type: Journal of Aircraft (ISSN 0021-8669); 26; 650-656
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  • 54
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    Validation of aerodynamic parameters for high-incidence research models (1989)
    In:  Other Sources
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    Publication Date: 2011-08-19
    Keywords: AERODYNAMICS
    Type: Journal of Aircraft (ISSN 0021-8669); 26; 621-628
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  • 55
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    Observation of airplane flowfields by natural condensation effects (1989)
    In:  Other Sources
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    Publication Date: 2011-08-19
    Keywords: AERODYNAMICS
    Type: Journal of Aircraft (ISSN 0021-8669); 26; 593-604
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  • 56
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    Separation control on an airfoil by periodic forcing (1989)
    In:  Other Sources
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    Publication Date: 2011-08-19
    Description: The introduction of transverse velocity fluctuations into a separated shear layer on an airfoil at high angles of attack is presently demonstrated to be an effective separation-control technique. Airfoil aerodynamic characteristics, including poststall lift and drag as well as maximum lift coefficient and stall angle, all exhibited improvements controlled forcing at 20 deg angle of attack led to an increased spreading of the mean velocity profile, together with increased turbulence activity; separation moved from the leading edge to about 80 percent of chord.
    Keywords: AERODYNAMICS
    Type: AIAA Journal (ISSN 0001-1452); 27; 820
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  • 57
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    Boundary-layer transition on a cone and flat plate at Mach 3.5 (1989)
    In:  Other Sources
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    Publication Date: 2011-08-19
    Keywords: AERODYNAMICS
    Type: AIAA Journal (ISSN 0001-1452); 27; 687-693
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  • 58
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    Full-potential analysis of a supersonic delta wing/body (1989)
    In:  Other Sources
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    Publication Date: 2011-08-19
    Keywords: AERODYNAMICS
    Type: Journal of Aircraft (ISSN 0021-8669); 26; 235-240
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  • 59
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    Direct simulation of three-dimensional hypersonic flow about intersecting blunt wedges (1989)
    In:  Other Sources
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    Publication Date: 2011-08-19
    Keywords: AERODYNAMICS
    Type: AIAA Journal (ISSN 0001-1452); 27; 1536-154
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  • 60
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    Turbulent separated flow over and downstream of a two-element airfoil (1989)
    In:  Other Sources
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    Publication Date: 2011-08-19
    Description: Flow characteristics in the vicinity of the flap of a single-slotted airfoil are presented and analyzed. The flow remained attached over the model surfaces, except in the vicinity of the flap trailing edge where a small region of boundary-layer separation extended over the aft 7 percent of flap chord. The airfoil configuration was tested at a Mach number of 0.09 and a chord Reynolds number of 1.8 x 10 to the 6th in the NASA Ames Research Center 7- by 10-Foot Wind Tunnel. The flow was complicated by the presence of a strong, initially inviscid, jet, emanating from the slot between airfoil and flap, and a gradual merging of the main airfoil wake and flap suction-side boundary layer.
    Keywords: AERODYNAMICS
    Type: Experiments in Fluids (ISSN 0723-4864); 7; 8, Se
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  • 61
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    Aerothermodynamic study of slender conical vehicles (1989)
    In:  Other Sources
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    Publication Date: 2011-08-19
    Keywords: AERODYNAMICS
    Type: Journal of Thermophysics and Heat Transfer (ISSN 0887-8722); 3; 361-367
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  • 62
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    Navier-Stokes computations of a prolate spheroid at angle of attack (1989)
    In:  Other Sources
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    Publication Date: 2011-08-19
    Keywords: AERODYNAMICS
    Type: Journal of Aircraft (ISSN 0021-8669); 26; 986-993
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  • 63
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    Application of transonic flow analysis to helicopter rotor problems (1989)
    In:  Other Sources
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    Publication Date: 2011-08-19
    Description: The transonic aspect of helicopter flow analysis is addressed. The equations of motion and their implementations are examined, and the computation of real rotor flows is considered. Nonlifting rotor flows, high-speed hover, high advance ratio lifting rotor flows, and strong blade/vortex interaction computations are discussed.
    Keywords: AERODYNAMICS
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  • 64
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    Basic numerical methods (1989)
    In:  Other Sources
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    Publication Date: 2011-08-19
    Description: Some of the basic finite-difference schemes that can be used to solve the nonlinear equations that describe unsteady inviscid and viscous transonic flow are reviewed. Numerical schemes for solving the unsteady Euler and Navier-Stokes, boundary-layer, and nonlinear potential equations are described. Emphasis is given to the elementary ideas used in constructing various numerical procedures, not specific details of any one procedure.
    Keywords: AERODYNAMICS
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  • 65
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    Numerical study of chemically reacting flows using a lower-upper symmetric successive overrelaxation scheme (1989)
    In:  Other Sources
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    Publication Date: 2011-08-19
    Keywords: AERODYNAMICS
    Type: AIAA Journal (ISSN 0001-1452); 27; 1752-176
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  • 66
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    Navier-Stokes computations of lee-side flows over delta wings (1989)
    In:  Other Sources
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    Publication Date: 2011-08-19
    Keywords: AERODYNAMICS
    Type: AIAA Journal (ISSN 0001-1452); 27; 1673-167
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  • 67
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    Laminar-flow flight experiments (1989)
    In:  CASI
    Details
    Publication Date: 2013-08-31
    Description: The flight testing conducted over the past 10 years in the NASA laminar-flow control (LFC) will be reviewed. The LFC program was directed towards the most challenging technology application, the high supersonic speed transport. To place these recent experiences in perspective, earlier important flight tests will first be reviewed to recall the lessons learned at that time.
    Keywords: AERODYNAMICS
    Type: Transonic Symposium: Theory, Application and Experiment, Volume 2; p 59-104
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  • 68
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    Laminar-flow wind tunnel experiments (1989)
    In:  CASI
    Details
    Publication Date: 2013-08-31
    Description: Although most of the laminar flow airfoils recently developed at the NASA Langley Research Center were intended for general aviation applications, low-drag airfoils were designed for transonic speeds and wind tunnel performance tested. The objective was to extend the technology of laminar flow to higher Mach and Reynolds numbers and to swept leading edge wings representative of transport aircraft to achieve lower drag and significantly improved operation costs. This research involves stabilizing the laminar boundary layer through geometric shaping (Natural Laminar Flow, NLF) and active control involving the removal of a portion of the laminar boundary layer (Laminar-Flow Control, LFC), either through discrete slots or perforated surface. Results show that extensive regions of laminar flow with large reductions in skin friction drag can be maintained through the application of passive NLF boundary-layer control technologies to unswept transonic wings. At even greater extent of laminar flow and reduction in the total drag level can be obtained on a swept supercritical airfoil with active boundary layer-control.
    Keywords: AERODYNAMICS
    Type: Transonic Symposium: Theory, Application and Experiment, Volume 2; p 105-145
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  • 69
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    Reynolds number effects on the transonic aerodynamics of a slender wing-body configuration (1989)
    In:  CASI
    Details
    Publication Date: 2013-08-31
    Description: Aerodynamic forces and moments for a slender wing-body configuration are summarized from an investigation in the Langley National Transonic Facility (NTF). The results include both longitudinal and lateral-directional aerodynamic properties as well as slideslip derivatives. Results were selected to emphasize Reynolds number effects at a transonic speed although some lower speed results are also presented for context. The data indicate nominal Reynolds number effects on the longitudinal aerodynamic coefficients and more pronounced effects for the lateral-directional aerodynamic coefficients. The Reynolds number sensitivities for the lateral-directional coefficients were limited to high angles of attack.
    Keywords: AERODYNAMICS
    Type: Transonic Symposium: Theory, Application and Experiment, Volume 2; p 41-58
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  • 70
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    A review of high-speed, convective, heat-transfer computation methods (1989)
    In:  CASI
    Details
    Publication Date: 2013-08-31
    Description: The objective is to provide useful engineering formulations and to instill a modest degree of physical understanding of the phenomena governing convective aerodynamic heating at high flight speeds. Some physical insight is not only essential to the application of the information presented here, but also to the effective use of computer codes which may be available to the reader. Given first is a discussion of cold-wall, laminar boundary layer heating. A brief presentation of the complex boundary layer transition phenomenon follows. Next, cold-wall turbulent boundary layer heating is discussed. This topic is followed by a brief coverage of separated flow-region and shock-interaction heating. A review of heat protection methods follows, including the influence of mass addition on laminar and turbulent boundary layers. Next is a discussion of finite-difference computer codes and a comparison of some results from these codes. An extensive list of references is also provided from sources such as the various AIAA journals and NASA reports which are available in the open literature.
    Keywords: AERODYNAMICS
    Type: Nielsen Engineering and Research, Inc., Missile Aerodynamics: NEAR Conference on Missile Aerodynamics; 64 p
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  • 71
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    Experience with some repeat tests on the 9 inch chord CAST-10-2/DOA 2 airfoil model in the Langley 0.3-m TCT adaptive wall test section (1989)
    In:  CASI
    Details
    Publication Date: 2013-08-31
    Description: A co-operative testing program is in progress between the Langley Research Center (NASA) and the National Aeronautical Establishment (NAE, Canada) to validate two different techniques of airfoil testing at transonic speeds. The procedure employed is to test the same airfoil model in the NAE two-dimensional tunnel and the Langley 0.3-m Transonic Cryogenic Tunnel (0.3-m TCT). The airfoil model used in testing was CAST-10-2/DOA-2 super-critical airfoil. The Langley 0.3-m TCT has a relatively small cross section of 13 in x 13 in, giving a (h/c) ratio of 1.44 for the same 9 in chord model. The approach employed in the 0.3-m TCT aims towards eliminating the wall effects by using active walls. The top and bottom walls are flexible. By changing the wall shapes during a test in an iterative manner, the wall interference effects are reduced. The method employed to change the wall shapes is the adaptive wall technique. The current test program provided an opportunity to validate the adaptive wall technique in the 0.3-m TCT. The relatively long chord airfoil represents a severe test case to test the efficacy of the adaptive wall technique under cryogenic conditions. The program also involved removal of side wall boundary-layer thus increasing the complexity of the wall adaptation technique. This paper deals with some salient results obtained regarding repeatability of test data and possible residual interference effects.
    Keywords: AERODYNAMICS
    Type: CAST-10-2(DOA 2 Airfoil Studies Workshop Results; p 213-231
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  • 72
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    Comparison of two- and three-dimensional Navier-Stokes solutions with NASA experimental data for CAST-10 airfoil (1989)
    In:  CASI
    Details
    Publication Date: 2013-08-31
    Description: The two-dimensional (2-D) and three-dimensional Navier-Stokes equations are solved for flow over a NAE CAST-10 airfoil model. Recently developed finite-volume codes that apply a multistage time stepping scheme in conjunction with steady state acceleration techniques are used to solve the equations. Two-dimensional results are shown for flow conditions uncorrected and corrected for wind tunnel wall interference effects. Predicted surface pressures from 3-D simulations are compared with those from 2-D calculations. The focus of the 3-D computations is the influence of the sidewall boundary layers. Topological features of the 3-D flow fields are indicated. Lift and drag results are compared with experimental measurements.
    Keywords: AERODYNAMICS
    Type: CAST-10-2(DOA 2 Airfoil Studies Workshop Results; p 233-258
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  • 73
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    An experimental AWTS process and comparisons of ONERA T2 and 0.3-m TCT AWTS data for the ONERA CAST-10 aerofoil (1989)
    In:  CASI
    Details
    Publication Date: 2013-08-31
    Description: An experimental Adaptive Wall Test Section (AWTS) process is described. Comparisons of the ONERA T2 and the 0.3-m TCT (transonic cryogenic tunnel) AWTS data for the ONERA CAST-10 airfoil are presented. Most of the 0.3-m TCT data is new and preliminary and no sidewall boundary layer control is involved. No conclusions are given.
    Keywords: AERODYNAMICS
    Type: CAST-10-2(DOA 2 Airfoil Studies Workshop Results; p 137-153
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  • 74
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    High Reynolds number tests of the CAST-10-2/DOA 2 transonic airfoil at ambient and cryogenic temper ature conditions (1989)
    In:  CASI
    Details
    Publication Date: 2013-08-31
    Description: The transonic airfoil CAST 10-2/DOA 2 was investigated in several major transonic wind tunnels at Reynolds numbers ranging from Re=1.3 x 10(exp 6) to 45 x 10(exp 6) at ambient and cryogenic temperature conditions. The main objective was to study the degree and extent of the effects of Reynolds number on both the airfoil aerodynamic characteristics and the interference effects of various model-wind-tunnel systems. The initial analysis of the CAST 10-2 airfoil results revealed appreciable real Reynolds number effects on this airfoil and showed that wall interference can be significantly affected by changes in Reynolds number thus appearing as true Reynolds number effects.
    Keywords: AERODYNAMICS
    Type: CAST-10-2(DOA 2 Airfoil Studies Workshop Results; p 47-60
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  • 75
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    Finite element flow-thermal-structural analysis of aerodynamically heated leading edges (1989)
    In:  CASI
    Details
    Publication Date: 2013-08-31
    Description: Hypersonic vehicles operate in a hostile aerothermal environment which has a significant impact on their aerothermostructural performance. Significant coupling occurs between the aerodynamic flow field, structural heat transfer, and structural response creating a multidisciplinary interaction. A long term goal of the Aerothermal Loads Branch at the NASA Langley Research Center is to develop a computational capability for integrated fluid, thermal and structural analysis of aerodynamically heated structures. The integrated analysis capability includes the coupling between the fluid and the structure which occurs primarily through the thermal response of the structure, because: (1) the surface temperature affects the external flow by changing the amount of energy absorbed by the structure, and (2) the temperature gradients in the structure result in structural deformations which alter the flow field and attendant surface pressures and heating rates. In the integrated analysis, a finite element method is used to solve: (1) the Navier-Stokes equations for the flow solution, (2) the energy equation of the structure for the temperature response, and (3) the equilibrium equations of the structure for the structural deformation and stresses.
    Keywords: AERODYNAMICS
    Type: Recent Advances in Multidisciplinary Analysis and Optimization, Part 2; p 971-990
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  • 76
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    Wall interference assessment and corrections (1989)
    In:  CASI
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    Publication Date: 2013-08-31
    Description: Wind tunnel wall interference assessment and correction (WIAC) concepts, applications, and typical results are discussed in terms of several nonlinear transonic codes and one panel method code developed for and being implemented at NASA-Langley. Contrasts between 2-D and 3-D transonic testing factors which affect WIAC procedures are illustrated using airfoil data from the 0.3 m Transonic Cryogenic Tunnel and Pathfinder 1 data from the National Transonic Facility. Initial results from the 3-D WIAC codes are encouraging; research on and implementation of WIAC concepts continue.
    Keywords: AERODYNAMICS
    Type: Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 2; p 817-851
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  • 77
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    Stability of compressible boundary layers (1989)
    In:  CASI
    Details
    Publication Date: 2013-08-31
    Description: The stability of compressible 2-D and 3-D boundary layers is reviewed. The stability of 2-D compressible flows differs from that of incompressible flows in two important features: There is more than one mode of instability contributing to the growth of disturbances in supersonic laminar boundary layers and the most unstable first mode wave is 3-D. Whereas viscosity has a destabilizing effect on incompressible flows, it is stabilizing for high supersonic Mach numbers. Whereas cooling stabilizes first mode waves, it destabilizes second mode waves. However, second order waves can be stabilized by suction and favorable pressure gradients. The influence of the nonparallelism on the spatial growth rate of disturbances is evaluated. The growth rate depends on the flow variable as well as the distance from the body. Floquet theory is used to investigate the subharmonic secondary instability.
    Keywords: AERODYNAMICS
    Type: NASA, Langley Research Center, Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 2; p 629-689
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    Turbulent eddy viscosity modeling in transonic shock/boundary-layer interactions (1989)
    In:  CASI
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    Publication Date: 2013-08-31
    Description: The treatment of turbulence effects on transonic shock/turbulent boundary layer interaction is addressed within the context of a triple deck approach valid for arbitrary practical Reynolds numbers between 1000 and 10 billion. The modeling of the eddy viscosity and basic turbulent boundary profile effects in each deck is examined in detail using Law-of-the-Wall/Law-of-the-Wake concepts as the foundation. Results of parametric studies showing how each of these turbulence model aspects influences typical interaction zone property distributions (wall pressure, displacement thickness and local skin friction) are presented and discussed.
    Keywords: AERODYNAMICS
    Type: NASA, Langley Research Center, Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 2; p 611-627
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  • 79
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    Airframe/propulsion integration characteristics at transonic speeds (1989)
    In:  CASI
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    Publication Date: 2013-08-31
    Description: The aerodynamic characteristics for both single and twin-engine high-performance aircraft are significantly affected by shock induced flow interactions as well as other local flow interference effects which usually occur at transonic speeds. These adverse interactions can not only cause high drag, but also cause unusual aerodynamic loadings and/or severe stability and control problems. Many programs are under way to not only develop method for reducing the adverse effects, but also to develop an understanding of the basic flow conditions which are the primary contributors. It is anticipated that these programs will result in technologies which can reduce the aircraft cruise drag through improved integration as well as increase aircraft maneuverability through the application of thrust vectoring. Some of the primary integration problems for twin-engine aircraft at transonic speeds are identified, and several methods are demonstrated for reducing or eliminating the undersirable characteristics, while enhancing configuration effectiveness.
    Keywords: AERODYNAMICS
    Type: Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 1; p 1-31
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  • 80
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    Generation of unstructured grids and Euler solutions for complex geometries (1989)
    In:  CASI
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    Publication Date: 2013-08-31
    Description: Algorithms are described for the generation and adaptation of unstructured grids in two and three dimensions, as well as Euler solvers for unstructured grids. The main purpose is to demonstrate how unstructured grids may be employed advantageously for the economic simulation of both geometrically as well as physically complex flow fields.
    Keywords: AERODYNAMICS
    Type: Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 1; p 377-408
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  • 81
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    Asymptotic methods for internal transonic flows (1989)
    In:  CASI
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    Publication Date: 2013-08-31
    Description: For many internal transonic flows of practical interest, some of the relevant nondimensional parameters typically are small enough that a perturbation scheme can be expected to give a useful level of numerical accuracy. A variety of steady and unsteady transonic channel and cascade flows is studied with the help of systematic perturbation methods which take advantage of this fact. Asymptotic representations are constructed for small changes in channel cross-section area, small flow deflection angles, small differences between the flow velocity and the sound speed, small amplitudes of imposed oscillations, and small reduced frequencies. Inside a channel the flow is nearly one-dimensional except in thin regions immediately downstream of a shock wave, at the channel entrance and exit, and near the channel throat. A study of two-dimensional cascade flow is extended to include a description of three-dimensional compressor-rotor flow which leads to analytical results except in thin edge regions which require numerical solution. For unsteady flow the qualitative nature of the shock-wave motion in a channel depends strongly on the orders of magnitude of the frequency and amplitude of impressed wall oscillations or fluctuations in back pressure. One example of supersonic flow is considered, for a channel with length large compared to its width, including the effect of separation bubbles and the possibility of self-sustained oscillations. The effect of viscosity on a weak shock wave in a channel is discussed.
    Keywords: AERODYNAMICS
    Type: NASA, Langley Research Center, Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 1; p 261-291
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  • 82
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    Euler solvers for transonic applications (1989)
    In:  CASI
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    Publication Date: 2013-08-31
    Description: The 1980s may well be called the Euler era of applied aerodynamics. Computer codes based on discrete approximations of the Euler equations are now routinely used to obtain solutions of transonic flow problems in which the effects of entropy and vorticity production are significant. Such codes can even predict separation from a sharp edge, owing to the inclusion of artificial dissipation, intended to lend numerical stability to the calculation but at the same time enforcing the Kutta condition. One effect not correctly predictable by Euler codes is the separation from a smooth surface, and neither is viscous drag; for these some form of the Navier-Stokes equation is needed. It, therefore, comes as no surprise to observe that the Navier-Stokes has already begun before Euler solutions were fully exploited. Moreover, most numerical developments for the Euler equations are now constrained by the requirement that the techniques introduced, notably artificial dissipation, must not interfere with the new physics added when going from an Euler to a full Navier-Stokes approximation. In order to appreciate the contributions of Euler solvers to the understanding of transonic aerodynamics, it is useful to review the components of these computational tools. Space discretization, time- or pseudo-time marching and boundary procedures, the essential constituents are discussed. The subject of grid generation and grid adaptation to the solution are touched upon only where relevant. A list of unanswered questions and an outlook for the future are covered.
    Keywords: AERODYNAMICS
    Type: NASA, Langley Research Center, Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 1; p 217-230
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  • 83
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    Transonics and fighter aircraft: Challenges and opportunities for CFD (1989)
    In:  CASI
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    Publication Date: 2013-08-31
    Description: The application of computational fluid dynamics (CFD) to fighter aircraft design and development is discussed. Methodology requirements for the aerodynamic design of fighter aircraft are briefly reviewed. The state-of-the-art of computational methods for transonic flows in the light of these requirements is assessed and the techniques found most adequate for the subject application are identified. Highlights from some proof-of-feasibility Euler and Navier-Stokes computations about a complete fighter aircraft configuration are presented. Finally, critical issues and opportunities for design application of CFD are discussed.
    Keywords: AERODYNAMICS
    Type: NASA, Langley Research Center, Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 1; p 153-173
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  • 84
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    Shock-boundary-layer interaction in flight (1989)
    In:  CASI
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    Publication Date: 2013-08-31
    Description: A brief survey is given on the study of transonic shock/boundary layer effects in flight. Then the possibility of alleviating the adverse shock effects through passive shock control is discussed. A Swedish flight experiment on a swept wing attack aircraft is used to demonstrate how it is possible to reduce the extent of separated flow and increase the drag-rise Mach number significantly using a moderate amount of perforation of the surface.
    Keywords: AERODYNAMICS
    Type: NASA, Langley Research Center, Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 1; p 61-77
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  • 85
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    Two-measured variable method for wall interference assessment/correction (1989)
    In:  CASI
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    Publication Date: 2013-08-31
    Description: An iterative method for wall interference assessment and/or correction is presented for transonic flow conditions in wind tunnels equipped with two component velocity measurements on a single interface. The iterative method does not require modeling of the test article and tunnel wall boundary conditions. Analytical proof for the convergence and stability of the iterative method is shown in the subsonic flow regime. The numerical solutions are given for both 2-D and axisymmetrical cases at transonic speeds with the application of global Mach number correction.
    Keywords: AERODYNAMICS
    Type: NASA, Langley Research Center, Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 2; p 853-866
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  • 86
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    Developments and trends in three-dimensional mesh generation (1989)
    In:  CASI
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    Publication Date: 2013-08-31
    Description: An intense research effort over the last few years has produced several competing and apparently diverse methods for generating meshes. Recent progress is reviewed and the central themes are emphasized which form a solid foundation for future developments in mesh generation.
    Keywords: AERODYNAMICS
    Type: NASA, Langley Research Center, Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 1; p 341-376
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  • 87
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    An embedded mesh procedure for leading-edge vortex flows (1989)
    In:  CASI
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    Publication Date: 2013-08-31
    Description: A cell-vertex scheme is outlined for solving the flow about a delta wing with M (sub infinity) is greater than 1. Embedded regions of mesh refinement allow solutions to be obtained which have much higher resolution than those achieved to date. Effects of mesh refinement and artificial viscosity on the solutions are studied, to determine at what point leading-edge vortex solutions are grid-converged. A macroscale and a microscale for the size of the vortex are defined, and it is shown that the macroscale (which includes the wing surface properties) is converged on a moderately refined grid, while the microscale is very sensitive to grid spacing. The level of numerical diffusion in the core of the vortex is found to be substantial. Comparisons with the experiment are made for two cases which have transonic cross-flow velocities.
    Keywords: AERODYNAMICS
    Type: NASA, Langley Research Center, Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 1; p 231-259
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  • 88
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    Computation of aircraft component flow fields at transonic Mach numbers using a three-dimensional Navier-Stokes algorithm (1989)
    In:  CASI
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    Publication Date: 2013-08-31
    Description: A computer analysis was developed for calculating steady (or unsteady) three-dimensional aircraft component flow fields. This algorithm, called ENS3D, can compute the flow field for the following configurations: diffuser duct/thrust nozzle, isolated wing, isolated fuselage, wing/fuselage with or without integrated inlet and exhaust, nacelle/inlet, nacelle (fuselage) afterbody/exhaust jet, complete transport engine installation, and multicomponent configurations using zonal grid generation technique. Solutions can be obtained for subsonic, transonic, or hypersonic freestream speeds. The algorithm can solve either the Euler equations for inviscid flow, the thin shear layer Navier-Stokes equations for viscous flow, or the full Navier-Stokes equations for viscous flow. The flow field solution is determined on a body-fitted computational grid. A fully-implicit alternating direction implicit method is employed for the solution of the finite difference equations. For viscous computations, either a two layer eddy-viscosity turbulence model or the k-epsilon two equation transport model can be used to achieve mathematical closure.
    Keywords: AERODYNAMICS
    Type: NASA, Langley Research Center, Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 1; p 175-194
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  • 89
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    Transonic CFD applications at Boeing (1989)
    In:  CASI
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    Publication Date: 2013-08-31
    Description: The use of computational methods for three dimensional transonic flow design and analysis at the Boeing Company is presented. A range of computational tools consisting of production tools for every day use by project engineers, expert user tools for special applications by computational researchers, and an emerging tool which may see considerable use in the near future are described. These methods include full potential and Euler solvers, some coupled to three dimensional boundary layer analysis methods, for transonic flow analysis about nacelle, wing-body, wing-body-strut-nacelle, and complete aircraft configurations. As the examples presented show, such a toolbox of codes is necessary for the variety of applications typical of an industrial environment. Such a toolbox of codes makes possible aerodynamic advances not previously achievable in a timely manner, if at all.
    Keywords: AERODYNAMICS
    Type: NASA, Langley Research Center, Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 1; p 79-107
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  • 90
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    Transition to turbulence in laminar hypersonic flow (1989)
    In:  CASI
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    Publication Date: 2013-08-31
    Description: Progress in a recently started project aimed at the prediction of transition to turbulence in hypersonic flow is briefly discussed. The prediction of transition to turbulence is a very important issue in the design of space vessels. Two space vehicles currently under investigation, namely the aeroassisted transfer vehicle (AOTV) and the trans-atmospheric vehicle (TAV), suffer from strong aerodynamic heating. This heating is strongly influenced by the boundary layer structure. These aerospace vehicles fly in the upper atmospheric layer at a Mach number between 10 and 30 at very low atmospheric pressures. At very high altitudes the flow is laminar, but when the space vessel returns to a lower orbit, the flow becomes turbulent and the heating is dramatically increased. The prediction of this transition process is commonly done by means of experiments. The experimental facilities available nowadays cannot model the hypersonic flow field accurately enough by limitations in Mach and Reynolds number. These facilities also have a large free stream disturbance level which makes it very difficult to investigate transition accurately. An alternative approach is to study transition by theoretical means. Up to now numerical studies of hypersonic flow only discussed steady laminar or turbulent flow. This theoretical approach is extended to the study of transition in hypersonic flow by means of direct numerical simulations and additional theoretical investigations to explain the mechanisms leading to transition. A brief outline of how this research is to be performed is given.
    Keywords: AERODYNAMICS
    Type: Annual Research Briefs, 1988; p 115-119
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  • 91
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    Computational aeroelasticity challenges and resources (1989)
    In:  CASI
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    Publication Date: 2013-08-31
    Description: In the past decade, there has been much activity in the development of computational methods for the analysis of unsteady transonic aerodynamics about airfoils and wings. Significant features are illustrated which must be addressed in the treatment of computational transonic unsteady aerodynamics. The flow regimes for an aircraft on a plot of lift coefficient vs. Mach number are indicated. The sequence of events occurring in air combat maneuvers are illustrated. And further features of transonic flutter are illustrated. Also illustrated are several types of aeroelastic response which were encountered and which offer challenges for computational methods. The four cases illustrate problem areas encountered near the boundaries of aircraft envelopes, as operating condition change from high speed, low angle conditions to lower speed, higher angle conditions.
    Keywords: AERODYNAMICS
    Type: Transonic Unsteady Aerodynamics and Aeroelasticity 1987, Part 2; p 631-637
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  • 92
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    Full potential unsteady computations including aeroelastic effects (1989)
    In:  CASI
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    Publication Date: 2013-08-31
    Description: A unified formulation is presented based on the full potential framework coupled with an appropriate structural model to compute steady and unsteady flows over rigid and flexible configurations across the Mach number range. The unsteady form of the full potential equation in conservation form is solved using an implicit scheme maintaining time accuracy through internal Newton iterations. A flux biasing procedure based on the unsteady sonic reference conditions is implemented to compute hyperbolic regions with moving sonic and shock surfaces. The wake behind a trailing edge is modeled using a mathematical cut across which the pressure is satisfied to be continuous by solving an appropriate vorticity convection equation. An aeroelastic model based on the generalized modal deflection approach interacts with the nonlinear aerodynamics and includes both static as well as dynamic structural analyses capability. Results are presented for rigid and flexible configurations at different Mach numbers ranging from subsonic to supersonic conditions. The dynamic response of a flexible wing below and above its flutter point is demonstrated.
    Keywords: AERODYNAMICS
    Type: NASA, Langley Research Center, Transonic Unsteady Aerodynamics and Aeroelasticity 1987, Part 1; p 175-191
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  • 93
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    Application of a full potential method to AGARD standard airfoils (1989)
    In:  CASI
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    Publication Date: 2013-08-31
    Description: One of the most important uses of method that calculate unsteady aerodynamic loads is to predict and analyze the aeroelastic responses of flight vehicles. Currently, methods based on transonic small disturbance potential aerodynamics are the primary tools for aeroelastic analysis. Flow solutions obtained using isentropic potential theory can be highly inaccurate and even multivalued, because they do not model the effects of entropy that is produced when shock waves are in the flow field. From the results that are presented, it is concluded that nonisentropic potential methods more accurately model Euler solutions than do isentropic methods. The primary effects of modeling shock generated entropy are: (1) to eliminate mulitple flow solutions when strong shock waves are in the flow field; and (2) to bring the strengths and locations of computed shock waves into better agreement with those calculated using Euler method and those measured during experiments.
    Keywords: AERODYNAMICS
    Type: Transonic Unsteady Aerodynamics and Aeroelasticity 1987, Part 1; p 157-174
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  • 94
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    Calculation of steady and unsteady pressures at supersonic speeds with CAP-TSD (1989)
    In:  CASI
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    Publication Date: 2013-08-31
    Description: A finite difference technique is used to solve the transonic small disturbance flow equation making use of shock capturing to treat wave discontinuities. Thus the nonlinear effects of thickness and angle of attack are considered. Such an approach is made feasible by the development of a new code called CAP-TSD (Computational Aeroelasticity Program - Transonic Small Disturbance), and is based on a fully implicit approximate factorization (AF) finite difference method to solve the time dependent transonic small disturbance equation. The application of the CAP-TSD code to the calculation of low to moderate supersonic steady and unsteady flows is presented. In particular, comparisons with exact linear theory solutions are made for steady and unsteady cases to evaluate shock capturing and other features of the current method. In addition, steady solutions obtained from an Euler code are used to evaluate the small disturbance aspects of the code. Steady and unsteady pressure comparisons are made with measurements for an F-15 wing model and for the RAE tailplane model.
    Keywords: AERODYNAMICS
    Type: Transonic Unsteady Aerodynamics and Aeroelasticity 1987, Part 1; p 117-137
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  • 95
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    Comparison of airfoil results from an adaptive wall test section and a porous wall test section (1989)
    In:  CASI
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    Publication Date: 2013-08-31
    Description: Two wind tunnel investigations were conducted to assess two different wall interference alleviation/correction techniques: adaptive test section walls and classical analytical corrections. The same airfoil model has been tested in the adaptive wall test section of the NASA-Langley 0.3 m Transonic Cryogenic Tunnel (TCT) and in the National Aeronautical Establishment (NAE) High Reynolds Number 2-D facility. The model has a 9 in. chord and a CAST 10-2/DOA 2 airfoil section. The 0.3 m TCT adaptive wall test section has four solid walls with flexible top and bottom walls. The NAE test section has porous top and bottom walls and solid side walls. The aerodynamic results corrected for top and bottom wall interference at Mach numbers from 0.3 to 0.8 at a Reynolds number of 10 by 1,000,000. Movement of the adaptive walls was used to alleviate the top and bottom wall interference in the test results from the NASA tunnel.
    Keywords: AERODYNAMICS
    Type: Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 2; p 867-890
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  • 96
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    An LDA (Laser-Doppler Anemometry) investigation of three-dimensional normal shock wave boundary-layer interactions (1989)
    In:  CASI
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    Publication Date: 2013-08-31
    Description: Nonintrusive measurements were made of a normal shock wave/boundary layer interaction. Two dimensional measurements were made throughout the interaction region while 3-D measurements were made in the vicinity of the shock wave. The measurements were made in the corner of the test section of a continuous supersonic wind tunnel in which a normal shock wave had been stabilized. Laser Doppler Anemometry, surface pressure measurement and flow visualization techniques were employed for two freestream Mach number test cases: 1.6 and 1.3. The former contained separated flow regions and a system of shock waves. The latter was found to be far less complicated. The results define the flow field structure in detail for each case.
    Keywords: AERODYNAMICS
    Type: NASA, Langley Research Center, Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 2; p 741-764
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  • 97
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    Secondary three-dimensional instability in compressible boundary layers (1989)
    In:  CASI
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    Publication Date: 2013-08-31
    Description: Three dimensional linear secondary instability theory is extended for compressible boundary layers on a flat plate in the presence of finite amplitude Tollmien-Schlichting waves. The focus is on principal parametric resonance responsible for strong growth of subharmonics in low disturbance environment.
    Keywords: AERODYNAMICS
    Type: NASA, Langley Research Center, Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 2; p 691-704
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  • 98
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    Turbulence and modeling in transonic flow (1989)
    In:  CASI
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    Publication Date: 2013-08-31
    Description: A review is made of the performance of a variety of turbulence models in the evaluation of a particular well documented transonic flow. This is done to supplement a previous attempt to calibrate and verify transonic airfoil codes by including many more turbulence models than used in the earlier work and applying the calculations to an experiment that did not suffer from uncertainties in angle of attack and was free of wind tunnel interference. It is found from this work, as well as in the earlier study, that the Johnson-King turbulence model is superior for transonic flows over simple aerodynamic surfaces, including moderate separation. It is also shown that some field equation models with wall function boundary conditions can be competitive with it.
    Keywords: AERODYNAMICS
    Type: NASA, Langley Research Center, Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 2; p 581-610
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  • 99
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    Euler/Navier-Stokes calculations of transonic flow past fixed- and rotary-wing aircraft configurations (1989)
    In:  CASI
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    Publication Date: 2013-08-31
    Description: Computational fluid dynamics has an increasingly important role in the design and analysis of aircraft as computer hardware becomes faster and algorithms become more efficient. Progress is being made in two directions: more complex and realistic configurations are being treated and algorithms based on higher approximations to the complete Navier-Stokes equations are being developed. The literature indicates that linear panel methods can model detailed, realistic aircraft geometries in flow regimes where this approximation is valid. As algorithms including higher approximations to the Navier-Stokes equations are developed, computer resource requirements increase rapidly. Generation of suitable grids become more difficult and the number of grid points required to resolve flow features of interest increases. Recently, the development of large vector computers has enabled researchers to attempt more complex geometries with Euler and Navier-Stokes algorithms. The results of calculations for transonic flow about a typical transport and fighter wing-body configuration using thin layer Navier-Stokes equations are described along with flow about helicopter rotor blades using both Euler/Navier-Stokes equations.
    Keywords: AERODYNAMICS
    Type: NASA, Langley Research Center, Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 2; p 521-545
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  • 100
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    Aerodynamic analysis of three advanced configurations using the TranAir full-potential code (1989)
    In:  CASI
    Details
    Publication Date: 2013-08-31
    Description: Computational results are presented for three advanced configurations: the F-16A with wing tip missiles and under wing fuel tanks, the Oblique Wing Research Aircraft, and an Advanced Turboprop research model. These results were generated by the latest version of the TranAir full potential code, which solves for transonic flow over complex configurations. TranAir embeds a surface paneled geometry definition in a uniform rectangular flow field grid, thus avoiding the use of surface conforming grids, and decoupling the grid generation process from the definition of the configuration. The new version of the code locally refines the uniform grid near the surface of the geometry, based on local panel size and/or user input. This method distributes the flow field grid points much more efficiently than the previous version of the code, which solved for a grid that was uniform everywhere in the flow field. TranAir results are presented for the three configurations and are compared with wind tunnel data.
    Keywords: AERODYNAMICS
    Type: NASA, Langley Research Center, Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 2; p 437-452
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