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  • Aerodynamics  (146)
  • Getreide
  • AERODYNAMICS
  • Animals
  • 1945-1949  (173)
  • 1925-1929
  • 1
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    Über Beziehungen zwischen der Witterung und den Ernteerträgen in Preußen (1926)
    In:  Landwirtschaftl. Jahrbuch 64:241-296
    Details
    Publication Date: 1926
    Description: Zusammenhang zwischen Niederschlag, Temperatur und Erträgen. Untersucht wurden Winterweizen, Winterroggen, Sommergerste, Sommerroggen, Kartoffeln, Futterpflanzen und Wiesen KATASTER-BESCHREIBUNG: Einfluss der Witterungsfaktoren Niederschlag und Temperatur auf die Ernteerträge KATASTER-DETAIL: Delta Nied +, dann Erträge (Halmfrüchte und Kartoffeln) + und später -; Delta T -, dann Erträge +,
    Keywords: Deutsches Reich (östl. u. westl. Provinzen, Hannover, Sachsen, Rheinland) ; 1899-1913 ; Ertrag ; Getreide ; Rangordnungsmethode ; Witterung ; Hackfrüchte
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  • 2
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    Korrelation zwischen Getreideernten und Monatssummen der Niederschläge in Baden (1926)
    In:  Diss.; Freiburg
    Details
    Publication Date: 1926
    Description: Abhängigkeit der Getreideerträge von Witterungseinflüssen mithilfe der Korrelationsmethode in 11 orographisch abgegrenzen Gebieten KATASTER-BESCHREIBUNG: Korrelation zwischen der Abweichung vom 11, bzw. 30jährigen monatlichen Mittel (April-Juli) der Niederschläge und dem Ertrag von Getreidearten (Weizen, Dinkel, Roggen, Gerste, Hafer) KATASTER-DETAIL: Nied 〉 (11, bzw. 30jährigen monatlichen Mittel von 1888-1898 und 1888-1917 im Monat Mai, je nach Region 55-158mm), dann höchste Übereinstimmung der Korrelationskoeffienten für die Ertragszunahme über alle Kulturen
    Keywords: Baden ; 1888-1898 und 1888-1917 ; Ertrag ; Getreide ; Korrelationsmethode ; Niederschlag ; Temperatur ; Witterung
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  • 3
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    Die konstitutionelle Anpassung der Kulturpflanzen an die Wasserversorgung (1949)
    In:  Zeitschrift für Pflanzenernährung, Düngung, Bodenkunde 46:176-190
    Details
    Publication Date: 1949
    Description: Zusammenhang zwischen Witterungsverlauf, Wasserbedarf und Erträgen, Aufstellung einer Konstitutionstheorie KATASTER-BESCHREIBUNG: Anpassung an den Wassermangel in der Jugend, Erziehung zur Dürreresistenz KATASTER-DETAIL: Wasserversorgung in der Jugend +, dann Wasserbedarf im Alter +;
    Keywords: Brandenburg ; 1946-48 ; Getreide ; Korrelationsmethode ; Temperatur ; Witterung
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  • 4
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    Die Abhängigkeit der Ernteerträge von den Witterungsfaktoren im Gebiet zwischen Saale, Mulde und Elbe (1928)
    In:  Vereinigten Friedrichs-Universität Halle-Wittenberg, Halle.
    Details
    Publication Date: 1928
    Description: Ertragsrelevante Korrelationen bei Winterweizen und -gerste mit der Temperatur, bei allen übrigen Kulturen war Niederschlag entscheidend KATASTER-BESCHREIBUNG: KATASTER-DETAIL:
    Keywords: Saalkreis, Kreis Bitterfeld, Kreis Delitzsch, Kreis Wittenberg, südl. Teil Kreis Köthen ; 1900-26 ; Kartoffeln ; Boden ; Ertrag ; Getreide ; Hafer ; Niederschlag ; Rangordnungsmethode ; Roggen ; Temperatur ; Weizen ; Witterung ; Hackfrüchte
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  • 5
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    Feldfrüchte und Witterung. (1949)
    In:  Deut. Landwirtschaflt. Presse 72:Nr. 3;6.
    Details
    Publication Date: 1949
    Description: Beziehung zwischen der Witterung und dem Ertrag verschiedener Kulturen KATASTER-BESCHREIBUNG: KATASTER-DETAIL:
    Keywords: Ostdeutschland ; 1900-1935 ; Boden ; Ertrag ; Getreide ; Witterung
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  • 6
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    Welchen Einfluss hat die ungünstige Witterung dieses Winters auf die Entwicklung unserer Kulturpflanzen? (1927)
    In:  Hannov. land- und forstw. Zeitg.:93-95
    Details
    Publication Date: 1927
    Description: Beschreibung der Witterungsverläufe der Winter und Empfehlungen für die Bodenbearbeitung und Bestandesführung von Winterkulturen KATASTER-BESCHREIBUNG: Einfluss der Witterung (Niederschlag und Temperatur) auf den Ertrag KATASTER-DETAIL: Delta Nied (Vorjahr) ++, dann Ertrag -; Delta Nied (Winter) +, dann Bodenfeuchte + und somit Ertrag +; Delta T (November) -, dann Ertrag -; Delta T (Winter) +, dann Ertrag +; Delta T (Frühling) +, dann Ertrag -;
    Keywords: Niedersachsen ; 1924-26 ; Insekten ; Ertrag ; Getreide ; Landwirtschaft ; Niederschlag ; Pflanzenschädling ; Roggen ; Weizen ; Düngung ; Gerste
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  • 7
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    Die Weißährigkeit des Weizens und ihre Ursachen (Ophiobolus herpotrichus u.a.) (1927)
    In:  Landwirtschaftliche Wochenschrift der Provinz Sachsen und Anhalt 29; p.668-670
    Details
    Publication Date: 1927
    Description: Der Autor führt aufgrund von Beobachtungen das Auftreten der Weißährigkeit auf Fußkrankheiten und Fusariumpilze, sowie landwirtschaftliche Praktiken zurück. In einem kleinen Abschnitt wird auch auf den Einfluß von Witterung und Bodenverhältnissen eingegangen. KATASTER-BESCHREIBUNG: KATASTER-DETAIL:
    Keywords: Sachsen, Sachsen-Anhalt ; 1926-1927 ; Getreide ; Pflanzenkrankheit ; Weizen
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  • 8
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    Tausendkorngewicht und Witterung in den Jahren 1921 bis 1926 (1928)
    In:  Georgine, Königsberg 104 (10):65-66
    Details
    Publication Date: 1928
    Description: Einluß von Temperatur und Niederschlag in bestimmten Zeiträumen auf das Tausendkorngewicht (TKG) KATASTER-BESCHREIBUNG: Zusammenhang Niederschlag, Temperatur und Sonnenscheinstunden zum Tausendkorngewicht (Ertrag) von Weizen, Roggen und Gerste KATASTER-DETAIL: Delta T (0,48-1,9°C während der Vegetationszeit April-August über dem Mittel der Jahre 1921-26) und Delta Nied (-25- +52% vom Schossen bis zur Ernte über dem Mittel der Jahre 1921-26), dann höhreres TKG um 11,6-21,4%
    Keywords: Pommern ; 1921-1926 ; Ertrag ; Getreide ; Niederschlag ; Roggen ; Temperatur ; Weizen ; Sonnenscheindauer ; Gerste
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  • 9
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    Eine Getreidelaufkäferplage (Zabru tenebrioides) (1925)
    In:  Die kranke Pflanze 2, p. 117-119
    Details
    Publication Date: 1925
    Description: Allgemeine Beobachtungen zum Auftreten und zur Wanderung des Getreidelaufkäfers und dessen Larven; Nennung von Möglichkeiten zur Bekämpfung des Insekts KATASTER-BESCHREIBUNG: Abhängigkeit der Stärke des Auftretens von der Temperatur KATASTER-DETAIL: Delta T+, dann Auftreten der Larven +
    Keywords: Sachsen ; Beginn 20. Jahrhundert ; Insekten ; Boden ; Ertrag ; Getreide ; Landwirtschaft ; Pflanzenschädling ; Roggen ; Temperatur ; Weizen
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  • 10
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    Die Ertragsbildung in Rekorderntejahren bei Getreide (1948)
    In:  Zeitschrift für Pflanzenernährung, Düngung, Bodenkunde 40:114-129.
    Details
    Publication Date: 1948
    Description: Beschreibung der Witterung innerhalb bestimmter Zeitabschnitte bei Rekordernten KATASTER-BESCHREIBUNG: Infolge von Wachstumshemmung, durch Trockenheit in der Jugend, und Transpirationseinschränkungen, durch ausbleibende Hitzeperioden im Alter, werden die, durch den Wechsel der Jahreszeiten gegebenen, starken Unterschiede in der Versorgung der Pflanzen wesentlich gemildert KATASTER-DETAIL: Delta Nied (März-April) -, dann Erträge ++; Delta T (März) + und Delta T (April) -, dann Erträge ++; Hitzeperioden (Mai-Juni) -, dann Erträge +; Delta T (Juli-August) + und Delta Nied (Juli-August)-, dann Erträge +; Trockenperioden (Juli-August) +, dann Erträge +;
    Keywords: Ostdeutschland ; 1929-38 ; Ertrag ; Getreide ; Niederschlag ; Temperatur ; Trockenheit ; Wachstum ; Witterung
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  • 11
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    Landwirtschaftlich-klimatologische Charakteristik Anhalts als Regenschattengebietes des Harzes (1929)
    In:  Buch von: Höhne, E., (1919): Landwirtschaftlich-klimatologische Untersuchung des Gebietes zwiwchen mittlerer Saale und Pleiße und Einteilung in klimatische Unterbezirke auf Grund der Beziehungen zwischen Witterungsfaktoren und Ernteerträgen
    Details
    Publication Date: 1929
    Description: Untersuchung zur Beziehung zwischen Witterungsfaktoren und Ernteerträgen in verschiedenen Untersuchungsgebieten mittels Rangordnungsdifferenzen. Betrachtet wurden die Erträge von Roggen, Winterweizen, Sommergerste, Hafer, Sommerweizen, Zuckerrübe, Kartoffel und Erbse KATASTER-BESCHREIBUNG: Einfluss der Witterung (Niederschlag, Temperatur, Sonnenschein) auf die Erträge KATASTER-DETAIL: Delta Nied (Oktober bis März) -, dann Erträge (Roggen) +; Delta Nied (Januar) -, dann Erträge (Roggen) ++; Delta Nied (Februar) +, dann Erträge (Roggen) +; Delta Nied (Mai) +, dann Erträge (Roggen) +; Delta Nied (Mai) 〉 1,5x Mittel, dann Erträge -; Delta Sonn (Mai, im Bezirk Köthen) +, dann Erträge (Roggen) -; Delta Nied (Januar, März, April) -, dann Erträge (Sommergerste) +; Delta Nied (Februar, Mai bis Ernte) +, dann Erträge (Sommergerste) +; Delta Nied (Mai) +, dann Erträge (Sommergerste) ++; Köthen (Nied 15-30mm im März), (Delta T- im April/Juni, besonders im Mai), dann Winterweizenertrag++ (weitere Informationen zu den weiteren landwirtschaftlicher Kulturpflanzen und Regionen: siehe Artikel)
    Keywords: Sachsen und Thüringen ; 1899-1926 ; Boden ; Ertrag ; Getreide ; Klima ; Korrelationsmethode ; Landwirtschaft ; Niederschlag ; Roggen ; Temperatur ; Weizen ; Globalstrahlung ; Hackfrüchte
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  • 12
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    Versuche über die Ausnützung steigender Stickstoffgaben durch verschiedene Hafersorten, IV Versuche mit Hafer (1929)
    In:  Zeitschrift für Pflanzenernährung, Düngung, Bodenkunde 8:425-458
    Details
    Publication Date: 1929
    Description: Auswirkungen über gestaffelte Stickstoff-Düngung auf den Ertrag von Weizen, Gerste, Roggen und Hafer. Angaben zu Temperatur und Niederschlag während der Vegetationszeit, Hinweise auf Zusammenhang zwischen Witterung und Ertrag und Wirkung der Düngung, Bedeutung eines längeren Zeitraums für die Beobachtungen KATASTER-BESCHREIBUNG: Einfluss von Niederschlag und Temperatur auf den Ertrag von Hafer KATASTER-DETAIL: Delta Nied (nach der Saat) +, dann t(Aufgang) - (später); Delta Nied (Ende des Wachstum) -, dann Erträge (Hafer) -; Delta T (20 Tage nach dem Aufgang) +: T 〉 11°C, dann Ertrag (Hafer) -;
    Keywords: Bayern ; 1924-28 ; Ertrag ; Getreide ; Hafer ; Niederschlag ; Roggen ; Temperatur ; Weizen ; Düngung ; Gerste
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  • 13
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    Beobachtungen über die diesjährige Dürre (1925)
    In:  Pflanzenbau, Halbmonatsschrift für Saatwesen, Anbau und Pflege der Kulturpflanzen. II. Jahrgang 1925/26 S.106-108.
    Details
    Publication Date: 1925
    Description: Einfluss der Trockenheit im Sommer auf Getreide, Leguminosen und Zuckerrüben KATASTER-BESCHREIBUNG: Einfluss der Temperatur und des Niederschlags auf den Ertrag KATASTER-DETAIL: Delta T (Vorjahreswinter) + und Delta Nied (Sommer) -, dann Pflanzenschädlinge (Erbsenwickler, Fritfliege) +; Delta T (Vorjahreswinter) + und Delta Nied (Sommer) -, dann Ertrag (Kartoffeln) +; Delta T (Vorjahreswinter) + und Delta Nied (Sommer) -, dann Ertrag (Sommergerste) -;
    Keywords: Pommern ; 1925 ; Ertrag ; Getreide ; Niederschlag ; Trockenheit
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  • 14
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    Die Beziehung zwischen Bodentemperatur und Lufttemperatur und ihrem Einfluss auf den Ernteertrag. (1927)
    In:  Fortschr. Landw. 2:205-212.
    Details
    Publication Date: 1927
    Description: Untersuchungen über die Gründe für die schlechte Getreideernte im Donau-Einzugsgebiet des Jahres 1924, Zusammenhang zwischen der Luft- und Bodentemperatur, dem Pflanzenwachtum und dem Ertrag KATASTER-BESCHREIBUNG: Korn-Stroh-Verhältnis wird beeinflusst von dem Verhältnis der Boden- zur Lufttemperatur, KATASTER-DETAIL: Delta T (Diff. Boden zu Luft im Mai) 〈 0, dann ertragsrelevant
    Keywords: Bayern ; 1913-15, 1924-26 ; Ertrag ; Getreide ; Temperatur ; Frost
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  • 15
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    Einfluss der Witterungs-Erscheinungen auf die Erträge unserer Kulturpflanzen. (1928)
    In:  Deut. Landwirtschaflt. Presse 55:94-95.
    Details
    Publication Date: 1928
    Description: Übersicht über die Literatur zum Einfluss des Wetters auf die Kulturpflanzen KATASTER-BESCHREIBUNG: Milder und trockener Winter wirkt positiv auf die Weizenerträge, kalter und niederschlagsreicher Winter eher negativ, Betrachung für Norddeutschland KATASTER-DETAIL:
    Keywords: Deutschland ; 1900-1926 ; Kartoffeln ; Ertrag ; Getreide ; Hafer ; Landwirtschaft ; Niederschlag ; Roggen ; Temperatur ; Trockenheit ; Witterung ; Gerste
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  • 16
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    Biometrical studies on the variation of physiologic forms of Puccinia graminis tritici and the effects of ecological factors on the susceptibility of wheat varieties (1928)
    In:  Phytopathology 18, No.1, p. 7-123
    Details
    Publication Date: 1928
    Description: Ergebnisse 5-jähriger Freilandversuche und 9-jähriger Laborversuche zu den Zusammenhängen zwischen klimatischen und anderen Umweltfaktoren und dem Auftreten verschiedener physiologischer Formen des Schwarzrostes an unterschiedlichen Weizensorten in den USA und Kanada. KATASTER-BESCHREIBUNG: KATASTER-DETAIL:
    Keywords: USA, Kanada ; 1919-1923 ; Getreide ; Pflanzenkrankheit ; Weizen
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  • 17
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    Zwei beachtenswerte Erscheinungen des Jahres 1926 (1926)
    In:  Hess. Landw. Zeitschr. 96, p.346
    Details
    Publication Date: 1926
    Description: Der Autor äußert die Vermutung, daß strenge Winter den Rostbefall vermindern und erwähnt das starke Befallsjahr 1926. Er klagt über ein noch zu geringes Wissen über die beeinflussenden Klimafaktoren. KATASTER-BESCHREIBUNG: KATASTER-DETAIL:
    Keywords: Wetterau, Hessen ; 1926 ; Getreide ; Pflanzenkrankheit
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  • 18
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    Frittfliegenbefall in den Ähren der Wintergerste (1949)
    In:  Neue Mitt. Landwirtsch. 4; p.130-132
    Details
    Publication Date: 1949
    Description: Der Autor beschreibt den Lebenszyklus der Frittfliege und dokumentiert das Auftreten des Schädlings in vergangenen Jahren. In einem sehr kurzen Absatz wird das Auftreten des schädlings mit warmem Frühlingswetter und der Sonnenscheindauer bzw. der Temperatur im Mai in Verbindung gebracht. KATASTER-BESCHREIBUNG: KATASTER-DETAIL:
    Keywords: Deutschland ; 1948 ; Getreide ; Pflanzenschädling ; Gerste
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  • 19
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    Massenauftreten der gelben Halmfliege in Schleswig-Holstein (1926)
    In:  Nachrichtenblatt für den deutschen Pflanzenschutzdienst, Jahrgang 6, Nr. 4, p. 27
    Details
    Publication Date: 1926
    Description: Beobachtungen zum Auftreten der gelben Halmfliege in Schleswig-Holstein und deren Auswirkungen auf bestimmte Getreidearten (Sommerweizen und Sommergerste) KATASTER-BESCHREIBUNG: Einfluss der Witterung auf das Auftreten der Fliege KATASTER-DETAIL: Delta Nied +, dann Sommerflug -
    Keywords: Schleswig-Holstein ; 1926 ; Insekten ; Anbautermine ; Getreide ; Landwirtschaft ; Niederschlag ; Pflanzenschädling ; Weizen ; Gerste
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  • 20
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    Korrelaionen zwischen Witterung und Ernteertrag (1945)
    In:  Verh. Schweiz. Naturforsch. Ges. Freiburg, 135-137
    Details
    Publication Date: 1945
    Description: Beziehung von Temperatur und Niederschlag zum Ertrag von Getreide KATASTER-BESCHREIBUNG: Anzahl der Tage mit Niederschlag im Juli (Korrelationskoeffizient =-0.6) hat höchste Korrelation bei Winterweizen KATASTER-DETAIL:
    Keywords: Schweiz ; 1942-44 ; Ertrag ; Getreide ; Korrelationsmethode ; Niederschlag ; Temperatur ; Weizen
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  • 21
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    Untersuchungen über Schadgebiet und Umweltfaktoren einiger landwirtschaftlicher Schädlinge in Deutschland auf Grund statistischer Unterlagen (1929)
    In:  Zeitschrift für angewandte Entomologie, Nov. 1929, p.565-627
    Details
    Publication Date: 1929
    Description: Einfluß der Witterung auf das Auftreten von Rübenaaskäfer, Zwergzikade, Ackerschnecke, Weizenhalmfliege, Getreideblumenfliege KATASTER-BESCHREIBUNG: KATASTER-DETAIL:
    Keywords: Deutschland, regional aufgelöst ; 1893-1927 ; Getreide ; Pflanzenschädling ; Hackfrüchte
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  • 22
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    Untersuchungen über die Beziehungen von Ernte- und Klimaschwankungen in der Wetterau (1948)
    In:  Diss., Gießen
    Details
    Publication Date: 1948
    Description: Rangordung der Ertrage nach Gruppen und Korrelationen zu Witterungsfaktoren; Ertragsaufzeichenungen von Betrieben und Klimaaufzeichnungen aus stat. Berichten der Wetterau KATASTER-BESCHREIBUNG: Ertragsrückgänge bei Wassermangel,Relation zwischen Ertrag und Temperatur/Luftfeuchte insb. bei Hackfrüchten KATASTER-DETAIL: Delta Nied (Herbst) -, Delta T (Winter) +, Delta T (Frühjahr) +, Delta Nied (Mai) +, Delta T (letzte Monate des Ausreifens) -, Delta Sonn (letzte Monate des Ausreifens) +, dann Ertrag +;
    Keywords: Wetterau, Hessen ; 1924-1938 ; Ertrag ; Getreide ; Niederschlag ; Temperatur ; Hackfrüchte
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  • 23
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    Erfahrungen über den diesjährigen Rostbefall beim Winterweizen und einige Vorbeugungsmaßnahmen (1926)
    In:  Jllustr. Landw. Zeitg. 46; p.551-552
    Details
    Publication Date: 1926
    Description: Schilderung des Rostbefalls (insbesondere Gelbrost)in der Region Kassel im Jahre 1926. Der Autor beklagt das bisher fehlende Wissen der Wissenschaftler und präsentiert eine Umfrage unter Landwirten zu den Einflußfaktoren (u.a. klimatische) auf den Rostbefall. Zudem werden Vorbeugungsmaßnahmen vorgestellt. KATASTER-BESCHREIBUNG: KATASTER-DETAIL:
    Keywords: Kassel ; 1926 ; Getreide ; Pflanzenkrankheit ; Weizen
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  • 24
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    Einfluß der Witterung auf die Entwicklung und den Gesundheitszustand der landwirtschaftlichen Kulturpflanzen im Jahre 1926 (1926)
    In:  Prakt. Blätter. Bayer. Landesanst. Pflanzenbau und Schutz 4 (5): 103-111
    Details
    Publication Date: 1926
    Description: Beobachtungen zu den Auswirkungen der Witterung im Jahr 1926 auf Getreide, Futterpflanzen und Kartoffeln sowie ihrer Schädigungen durch verschiedene Schaderreger, wie z.B. Roste, Fusarien, Phytophthora, etc. KATASTER-BESCHREIBUNG: Einfluss der Witterung (Temperatur, Niederschlag, Sonnenschein) auf den Ertrag KATASTER-DETAIL: Delta T (Februar) +, dann Auswinterungsschäden +; Delta T (März, April) + und Delta Nied (März) +, dann Entwicklung + (früher); Delta T (Mai, Juni) -: T 〈 0 °C (Frost), dann Kälteschäden +; Delta Sonn (Juni, Juli) -, dann Entwicklung -; Delta T (Frühjahr) +, dann Ertrag (Wintergetreide - außer Winterroggen) +; Delta T (Mai) - : T 〈 0 °C, dann Wachstum (Winterweizen) - und Auftreten von Gelbrost +, dadurch Ertrag (Winterweizen) -; Delta T(Frühjahr) +, dann Saat + (früher) und Entwicklung +, dadurch Ertrag (Sommergetreide) +; Delta Nied (Sommer) +, dann Entwicklung (Rüben) +; Delta Nied (Sommer) + und Delta T (Sommer) -, dann Entwicklung (Pferdebohnen) -; Delta Nied (Sommer) + und Delta T (Sommer) -, dann Entwicklung (Kartoffeln) -;
    Keywords: Bayern ; 1926 ; Kartoffeln ; Getreide ; Pflanzenkrankheit ; Pflanzenschädling ; Hackfrüchte
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  • 25
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    Witterung und Gerstenerträge (1928)
    In:  Landw. Wochenschrift für die Provinz Sachsen und Anhalt, Hallle 18:428ff.
    Details
    Publication Date: 1928
    Description: Zusammenhang Witterung in Monaten und Gerstenertrag KATASTER-BESCHREIBUNG: KATASTER-DETAIL:
    Keywords: Sachsen und Anhalt ; 1920 ; Ertrag ; Getreide ; Landwirtschaft ; Niederschlag ; Temperatur ; Witterung
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  • 26
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    Der Einfluß des Klimas auf die Erntebeschaffenheit des Getreides (1925)
    In:  Mitt. Deut. Landw. Gesell. 40:950-55.
    Details
    Publication Date: 1925
    Description: Zusammenhang zwischen Weizenqualität und den klimatischen Verhältnissen, Schwerpunkt auf die Physiologie des Samens und Qualität (Backfähigkeit) KATASTER-BESCHREIBUNG: KATASTER-DETAIL:
    Keywords: Europa ; letzten100 Jahre ; Ertrag ; Getreide ; Klima ; Niederschlag ; Temperatur ; Weizen
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  • 27
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    Untersuchungen über Beziehungen zwischen Witterung und Ernteertrag in der Landwirtschaft (1928)
    In:  Diss., Hohenheim.
    Details
    Publication Date: 1928
    Description: Beziehung zwischen Witterung (unterteilt in einzelne Monate) und Ertragshöhe mithilfe der Rangordnungs- und der Korrelationsmethode KATASTER-BESCHREIBUNG: Einfluss der Witterung (Temperatur, Niederschlag, Sonnenscheindauer) auf den Ertrag von Winterweizen, Sommerweizen, Sommergerste, Wintergerste, Hafer und Runkelrüben auf dem Versuchsfeld (wasserundurchlässiger Boden) KATASTER-DETAIL: Delta Sonn (Oktober bis November)+, dann Erträge (Winterweizen) +; Delta Sonn (Dezember bis März)+, dann Erträge (Winterweizen) -; Delta Sonn (April) -, dann Erträge (Winterweizen) +; Delta Nied (April) +, dann Erträge (Winterweizen) +; Delta Nied (Mai, Juni und Juli) -, dann Erträge (Winterweizen) +; Delta Nied (August bis Oktober) +, dann Erträge (Winterweizen) +; Delta T (April) -, dann Erträge (Winterweizen) +; (Details sowie Informationen für Sommerweizen, Sommergerste, Wintergerste, Hafer und Runkelrüben siehe Artikel)
    Keywords: Hohenheim (Baden-Württemberg) ; 1914-25 ; Ertrag ; Getreide ; Hafer ; Klima ; Korrelationsmethode ; Niederschlag ; Rangordnungsmethode ; Temperatur ; Weizen ; Witterung ; Hackfrüchte
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  • 28
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    Die "kritischen Zeiten" und das "ökologische Optimum" der Witterungsfaktoren, ein Mittel zur Bestimmung der Ernteertäge (1926)
    In:  Zeitschrift für Acker- und Pflanzenbau 3:330-334.
    Details
    Publication Date: 1926
    Description: Angabe von Niederschlagsmengen und Durchschnittstemperaturen für das ökologische Optimum bestimmter Sorten, kritische Zeiten (vor und nach der Blüte) sind hierfür entscheidend KATASTER-BESCHREIBUNG: Einfluss von Wasser und Wärme, bzw. Niederschlag und Temperatur auf den Ertrag KATASTER-DETAIL: Roggen, Weizen: Delta Nied (Beginn Blütezeit)-, dann Ertrag +; Hafer, Gerste, Kartoffel: Delta T (Beginn der Blüte) -, dann Ertrag +; Bohne: Delta T (gesamte Wachstumszeit)+ und Delta Nied (gesamte Wachstumszeit) +, dann Ertrag +
    Keywords: Göttingen ; 1901-22 ; Kartoffeln ; Ertrag ; Getreide ; Hafer ; Klima ; Korrelationsmethode ; Niederschlag ; Roggen ; Temperatur ; Weizen ; Witterung ; Hackfrüchte ; Erbsen
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  • 29
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    Zwei verbreitete Weizenschädlinge dieses Jahres (1925)
    In:  Sächs. Landw. Zeitschr. 73, p.614
    Details
    Publication Date: 1925
    Description: Beschreibung der Schäden und Erscheinungsformen des Weizenhalmtöters und der Weizenhalmfliege im Jahre 1926 in Sachsen. Nur bedingte Verknüpfung mit klimatischen Parametern. KATASTER-BESCHREIBUNG: KATASTER-DETAIL:
    Keywords: Sachsen ; 1926 ; Getreide ; Pflanzenschädling ; Weizen
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  • 30
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    Die Schwankungen der barometrischen Hochlagen über Mitteleuropa und ihr Einfluß auf die Ernteerträge in Deutschland (1929)
    In:  Kühn-Archiv, Berlin, XX, Seite 7-129
    Details
    Publication Date: 1929
    Description: Lage der Hochs nördlich und südlich des 50. Breitengrades und ihre Bedeutung für die Witterung und Ernteerträge in Mitteldeutschland KATASTER-BESCHREIBUNG: KATASTER-DETAIL: Tmit+ (Janurar, Februar, März, Mai und Dezember) durch Abnahem der barometrischen Nordlagen Tmit- (August, September) durch Zunahme der barometrischen Nordlagen Nied+ (Janurar, Apri,, Mai, August, September, Dezember) durch Abnahmen der barometrischen Nordlagen (entspricht Zunahmen der Südlagen!) Nied- (Februar, März, Oktober und November) durch Abnahmen der barometrischen Nordlagen (entspricht Zunahmen der Südlagen!)
    Keywords: Deutschland ; 1900-1925 ; Luftfeuchte ; Ertrag ; Getreide ; Landwirtschaft ; Niederschlag ; Temperatur ; Trockenheit ; Witterung ; Sonnenscheindauer
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  • 31
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    Insektenschädigungen am Getreide (1925)
    In:  Georgine, Jahrgang 102, Nr. 68, p. 806-807
    Details
    Publication Date: 1925
    Description: Biologie und Bekämpfung von Fritfliege, Getreideblumenfliege, scheckige oder gelbe Halmfliege, Weizenfliege, Hessenfliege KATASTER-BESCHREIBUNG: Einfluss der Witterung (Temperatur, Niederschlag und Wind) auf die Schädlinge KATASTER-DETAIL: Delta T (Winter) +, Anzahl Maden der Halmfliege +; Delta Nied (September) + und Delta Wind (September) +, dann Hessenfliege -
    Keywords: Deutschland ; 1903-1925 ; Insekten ; Anbautermine ; Boden ; Ertrag ; Getreide ; Hafer ; Niederschlag ; Pflanzenschädling ; Temperatur ; Vegetationsperiode ; Weizen ; Wind ; Witterung ; Düngung ; Gerste
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  • 32
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    Zum Auftreten des Gelbrostes des Weizens (1926)
    In:  Nassauer Land 108, p. 185
    Details
    Publication Date: 1926
    Description: Beobachtungen zum Gelbrostbefall von Weizen, Roggen und Gerste KATASTER-BESCHREIBUNG: - KATASTER-DETAIL: -
    Keywords: Deutschland ; 1926 ; Infektionskrankheiten ; Getreide ; Pflanzenkrankheit ; Roggen ; Weizen ; Gerste
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  • 33
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    Die Ertragsbildung in Rekorderntejahren bei Getreide (1948)
    In:  Zeitschr. Pflanzenernährung, Düngung, Bodenkunde 40: 114-129
    Details
    Publication Date: 1948
    Description: Vergleich der Witterungsfaktoren in den Rekorderntejahren 1933 und 1938 von März bis August KATASTER-BESCHREIBUNG: Identifizierung der wichtigen Zeitabschnitte März-April und Juli-August,hier hohe Temperaturen für Rekordernten unabdingbar KATASTER-DETAIL: Delta Nied - (Frühjahr), dann Ertrag +; Nied (Normal und gleichmäßig), im Mai Delta Nied+, dann Ertrag+
    Keywords: Berlin, Brandenburg ; 1933-1938 ; Ertrag ; Getreide ; Niederschlag ; Temperatur ; Trockenheit
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  • 34
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    NACA Conference on Boundary Layers. A compilation of the papers presented (1947)
    In:  Other Sources
    Details
    Publication Date: 2011-08-17
    Keywords: AERODYNAMICS
    Format: text
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  • 35
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    Lattice arrangements for rapid convergence (1926)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Description: A simple, systematic, optimized vortex-lattice approach is developed for application to lifting-surface problems. It affords a significant reduction in computational costs when compared to current methods. Extensive numerical experiments have been carried out on a wide variety of configurations, including wings with camber and single or multiple flaps, as well as high-lift jetflap systems. Rapid convergence as the number of spanwise or chordwise lattices are increased is assured, along with accurate answers. The results from this model should be useful not only in preliminary aircraft design but also, for example, as input for wake vortex roll-up studies and transonic flow calculations.
    Keywords: AERODYNAMICS
    Type: NASA. Langley Res. Center Vortex-Lattice Utilization; p 325-342
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  • 36
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    Some considerations of aerodynamic heating (1948)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Keywords: AERODYNAMICS
    Type: NACA: Univ. Conf. on Aerodyn.; p 399-411
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  • 37
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    The use of conincal and cylindrical fields in supersonic wing theory (1948)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Keywords: AERODYNAMICS
    Type: NACA. Langley Aeron. Lab. NACA: Univ. Conf. on Aerodyn.; p 341-353
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  • 38
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    Summary of NACA submerged-inlet investigations (1947)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Keywords: AERODYNAMICS
    Type: NACA Conf. on Aerodyn. Probl. of Transonic Airplane Design; p 49-52
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  • 39
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    Lift and drag characteristics of a wing with several angles of sweep at high subsonic speeds (1947)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Keywords: AERODYNAMICS
    Type: NACA. Ames Aeron. Lab. NACA Conf. on Aerodyn. Probl. of Transonic Airplane Design; p 21-28
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  • 40
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    Investigation of side inlets at supersonic speeds (1947)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Keywords: AERODYNAMICS
    Type: NACA Conf. on Aerodyn. Probl. of Transonic Airplane Design; p 53-57
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  • 41
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    A review of recent information relating to the drag rise of airplanes (1947)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Keywords: AERODYNAMICS
    Type: NACA. Ames Aeron. Lab. NACA Conf. on Aerodyn. Probl. of Transonic Airplane Design; p 3-13
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  • 42
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    Air inlets (1948)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Keywords: AERODYNAMICS
    Type: NACA: Univ. Conf. on Aerodyn.; p 307-322
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  • 43
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    Characteristics of wing sections at transonic speeds (1948)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Keywords: AERODYNAMICS
    Type: NACA: Univ. Conf. on Aerodyn.; p 127-149
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  • 44
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    A review of approximate methods in subsonic compressible flow (1948)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Keywords: AERODYNAMICS
    Type: NACA: Univ. Conf. on Aerodyn.; p 29-46
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  • 45
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    The use of source and sink concepts in the calculation of wing characteristics at supersonic speeds (1948)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Keywords: AERODYNAMICS
    Type: NACA: Univ. Conf. on Aerodyn.; p 355-365
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  • 46
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    Prediction of Wing Characteristics (1948)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Keywords: AERODYNAMICS
    Type: NACA: Univ. Conf. on Aerodyn.; p 151-166
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  • 47
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    Characteristics of wing sections at subcritical speeds (1948)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Keywords: AERODYNAMICS
    Type: NACA: Univ. Conf. on Aerodyn.; p 109-125
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  • 48
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    Two-dimensional supersonic wing theory (1948)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Keywords: AERODYNAMICS
    Type: NACA. Langley Aeron. Lab. NACA: Univ. Conf. on Aerodyn.; p 325-340
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  • 49
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    Prediction of the aerodynamic characteristics of wings of arbitrary plan form (1947)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Keywords: AERODYNAMICS
    Type: NACA Conf. on Aerodyn. Probl. of Transonic Airplane Design; p 95-100
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  • 50
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    Nose inlets (1947)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Keywords: AERODYNAMICS
    Type: NACA. Ames Aeron. Lab. NACA Conf. on Aerodyn. Probl. of Transonic Airplane Design; p 43-48
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  • 51
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    Airfoil section characteristics at high subsonic speeds (1947)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Keywords: AERODYNAMICS
    Type: NACA Conf. on Aerodyn. Probl. of Transonic Airplane Design; p 15-20
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  • 52
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    A survey of methods for the calculation of flow around bodies of revolution at supersonic speeds (1948)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Keywords: AERODYNAMICS
    Type: NACA: Univ. Conf. on Aerodyn.; p 377-395
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  • 53
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    Unsteady lift in high-speed flight (1948)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Keywords: AERODYNAMICS
    Type: NACA. Langley Aeron. Lab. NACA: Univ. Conf. on Aerodyn.; p 367-376
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  • 54
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    Maximum-lift and stalling characteristics of wings (1948)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Keywords: AERODYNAMICS
    Type: NACA: Univ. Conf. on Aerodyn.; p 167-183
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  • 55
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    Stability of the laminar boundary layer (1948)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Keywords: AERODYNAMICS
    Type: NACA: Univ. Conf. on Aerodyn.; p 3-26
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  • 56
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    High Speed Wind-Tunnel Investigation of the Longitudinal Stability and Control Characteristics of a 1/16-Scale Model of the D-558-2 Research Airplane at High Subsonic Mach Number and at a Mach Number of 1.2 (1949)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: No abstract available
    Keywords: Aerodynamics
    Type: NACA-RM-L9C04
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  • 57
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    An Analysis of the Effects of Wing Aspect Ratio and Tail Location on Static Longitudinal Stability Below the Mach Number of Lift Divergence (1948)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: An analysis is presented of the influence of wing aspect ratio and tail location on the effects of compressibility upon static longitudinal stability. The investigation showed that the use of reduced wing aspect ratios or short tail lengths leads to serious reductions in high-speed stability and the possibility of high-speed instability.
    Keywords: Aerodynamics
    Type: NACA-RM-A7J13
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  • 58
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    Investigation of Pressure Distribution over an Extended Leading-Edge Flap on a 42 Degrees Sweptback Wing (1947)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Pressure distribution over an extended leading-edge flap on a 42 degree swept-back wing was investigated. Results indicate that the flap normal-force coefficient increased almost linearly with the angle of attack to a maximum value of 3.25. The maximum section normal-force coefficient was located about 30 percent of the flap span outboard of the inboard end and had a value of 3.75. Peak negative pressures built up at the flap leading edge as the angle of attack was increased and caused the chordwise location of the flap center of pressure to be move forward.
    Keywords: Aerodynamics
    Type: NACA-RM-L7J03
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  • 59
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    Investigation of Thrust Augmentation of a 1600-pound Thrust Centrifugal-flow-type Turbojet Engine by Injection of Refrigerants at Compressor Inlets (1947)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Investigations were conducted to determine effectiveness of refrigerants in increasing thrust of turbojet engines. Mixtures of water an alcohol were injected for a range of total flows up to 2.2 lb/sec. Kerosene was injected into inlets covering a range of injected flows up to approximately 30% of normal engine fuel flow. Injection of 2.0 lb/sec of water alone produced an increase in thrust of 35.8% of rate engine conditions and kerosene produced a negligible increase in thrust. Carbon dioxide increased thrust 23.5 percent.
    Keywords: Aerodynamics
    Type: NACA-RM-E7G23
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  • 60
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    Observations on an Aileron-Flutter Instability Encountered on a 45 Degree Swept-Back Wing in Transonic and Supersonic Flight (1947)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: In the course of a flight test of a supersonic research pilotless aircraft (the NACA RM-1), large-amplitude aileron oscillations, probably aileron compressibility flutter, were encountered in the transonic and supersonic speed ranges. The wing was oscillating at the same frequency as the aileron. The aircraft was equipped with 45 degree swept-back wings of symmetrical NASA 65-010 airfoil section. Completely mass-balanced ailerons with 20 degree beveled trailing edges were installed on the wings. The ailerons were free floating with no mechanical restraining force other than the friction of the aileron hinges and servomechanism bearings throughout the high-speed interval of flight.
    Keywords: Aerodynamics
    Type: NACA-RM-L6L09
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  • 61
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    High-Speed Wind-Tunnel Investigation of the Lateral Control Characteristics of Plain Ailerons on a Wing with Various Amounts of Sweep (1947)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: A three-dimensional investigation of straight-sided-profile plain ailerons on a wing with 30 degrees and 45 degrees of sweepback and sweepforward was made in a high-speed wind tunnel for aileron deflections from -10 degrees to 10 degrees and at Mach numbers from 0.60 to 0.96. Wing configurations of 30 degrees generally reduced the severity of the large changes in rolling-moment and aileron hinge-moment coefficients experienced by the upswept wing configurations as the result of compression shock and extended to higher Mach numbers the speeds at which such changes occurred.
    Keywords: Aerodynamics
    Type: NACA-RM-L7I15
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  • 62
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    Calculations of the Supersonic Wave Drag of Nonlifting Wings with Arbitrary Sweepback and Aspect Ratio: Wings Swept Behind the Mach Lines (1947)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: On the basis of a recently developed theory for finite sweptback wings at supersonic speeds, calculations of the supersonic wave drag at zero lift were made for a series of wings having thin symmetrical biconvex sections with untapered plan forms and various angles of sweepback and aspect ratios. The results are presented in a unified form so that a single chart permits the direct determination of the wave drag for this family of airfoils for an extensive range of aspect ratio and sweepback angle for stream Mach numbers up to a value corresponding to that at which the Mach line coincides with the wing leading edge. The calculations showed that in general the wave-drag coefficient decreased with increasing sweepback. At Mach numbers for which the Mach lines are appreciably ahead of the wing leading edge, the 'wave-drag coefficient decreased to an important extent with increases in aspect ratio or slenderness ratio. At Mach numbers for which the Mach lines approach the wing leading edge (Mach numbers approaching a value equal to the secant of the angle of sweepback), the wave-drag coefficient decreased with reductions in aspect ratio or slenderness ratio. In order to check the results obtained by the theory, a comparison was made with the results of tests at the Langley Memorial Aeronautical Laboratory of sweptback wing attached to a freely falling body. The variation of the drag with Mach number and aspect ratio as given by the theory appeared to be in reasonable
    Keywords: Aerodynamics
    Type: NACA-RM-L6K29
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  • 63
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    Measurements of Static and Total Pressure Throughout the Transonic Speed Range as Obtained from an Airspeed Head Mounted on a Freely Falling Body (1947)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: No abstract available
    Keywords: Aerodynamics
    Type: NACA-RM-L7C04a
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  • 64
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    An Investigation of Convergent-Divergent Diffusers at Mach Number 1.85 (1947)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: An investigation has been conducted in the Cleveland 18- by 18-inch supersonic tunnel at a Mach number of 1.85 and angles of attack from 0 deg to 5 deg to determine optimum design configurations for a convergent-divergent type of supersonic diffuser with a subsonic diffuser of 5 deg included divergence angle. Total pressure recoveries in excess of theoretical recovery across a normal shock at a free-stream Mach number of 1.85 wore obtained with several configurations. The highest recovery for configurations without a cylindrical throat section was obtained with an inlet having an included convergence angle of 20 deg. Insertion of a 2-inch throat section between a 10 deg included angle inlet and the subsonic diffuser stabilized the shock inside the diffuser and resulted in recoveries as high as 0.838 free-stream total pressure at an angle of attack of 0 deg, corresponding to recovery of 92.4 percent of the kinetic energy of the free air stream. Use of the throat section also lessened the reduction in recovery of all configurations due to angle of attack.
    Keywords: Aerodynamics
    Type: NACA-RM-E6K21
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  • 65
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    Effects of Mach Number and Reynolds Number on the Maximum Lift Coefficient of a Wing of NACA 230-series Airfoil Sections (1947)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Wing was tested with full-span, partial-span, or split flaps deflected 60 Degrees and without flaps. Chordwise pressure-distribution measurements were made for all flap configurations.. Peak values of maximum lift coefficient were obtained at relatively low free-stream Mach numbers and, before critical Mach number was reached, were almost entirely dependent on Reynolds Number. Lift coefficient increased by increasing Mach number or deflecting flaps while critical pressure coefficient was reached at lower free-stream Mach numbers.
    Keywords: Aerodynamics
    Type: NACA-TN-1299
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  • 66
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    A Comparison of the Lateral Motion Calculated for Tailless and Conventional Airplanes (1947)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Theoretical analysts of lateral dynamic motion of tailless and conventional airplanes was made for fighter and heavy transport. Their reactions to a lateral gust and control power required by each for simple maneuvers were determined and compared. Both types of airplanes require almost identical aileron control power to perform a given maneuver; tailless airplane requires about 1-2 to 1-3 directional control power of conventional airplane. Tailless airplane also shows greatest displacement for a given disturbance and has least damping in oscillatory mode.
    Keywords: Aerodynamics
    Type: NACA-TN-1154
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  • 67
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    Effect of the NACA Injection Impeller on the Mixture Distribution of a Double-row Radial Aircraft Engine (1946)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: For the normal range of engine power the impeller provided marked improvement over the standard spray-bar injection system. Mixture distribution at cruising was excellent, maximum cylinder temperatures were reduced about 30 degrees F, and general temperature distribution was improved. The uniform mixture distribution restored the normal response of cylinder temperature to mixture enrichment and it reduced the possibility of carburetor icing, while no serious loss in supercharger pressure rise resulted from injection of fuel near the impeller outlet. The injection impeller also furnished a convenient means of adding water to the charge mixture for internal cooling.
    Keywords: Aerodynamics
    Type: NACA-TN-1069
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  • 68
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    Correlation Tests of the Ditching Behavior of an Army B-24D Airplane and a 1/16-size Model (1946)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Behaviors of both model and full-scale airplanes were ascertained by making visual observations, by recording time histories of decelerations, and by taking motion picture records of ditchings. Results are presented in form of sequence photographs and time-history curves for attitudes, vertical and horizontal displacements, and longitudinal decelerations. Time-history curves for attitudes and horizontal and vertical displacements for model and full-scale tests were in agreement; maximum longitudinal decelerations for both ditchings did not occur at same part of run; full-scale maximum deceleration was 50 percent greater.
    Keywords: Aerodynamics
    Type: NACA-WR-L-617 , NACA-MR-L6A03
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  • 69
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    Numerical Evaluation by Harmonic Analysis of the (Epsilon)-Function of the Theodorsen Arbitrary-Airfoil Potential Theory (1945)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Finite trigonometric series is fitted by harmonic analysis as an approximation function to the psi function of the Theodorsen arbitrary-airfoil potential theory. By harmonic synthesis, the corresponding conjugate trigonometric series is used as an approximation to the epsilon function. A set of coefficients of particularly simple form is obtained algebraically for direct calculation of the epsilon values from the corresponding set of psi values. Complete derivation of this process is presented.
    Keywords: Aerodynamics
    Type: NACA-WR-L-153 , NACA-ARR-L5H18
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  • 70
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    The Effect of Afterbody Length of the Hydrodynamic Stability of a Dynamic Model of a Flying Boat: Langley Tank Model 134 (1945)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: A program of model tests has been completed at Langley tank no. 1 which will furnish a qualitative guide as to the relation of length of afterbody and depth of step. The model used for the tests was a l/12-size unpowered dynamic model of a hypothetical 160,000-pound airplane. The results showed that an increase in length of afterbody requires an accompanying increase in depth of step to maintain adequate landing stability. Changing the length of afterbody and depth of step in such a manner as to maintain a given landing stability will result in only small changes in take-off stability.
    Keywords: Aerodynamics
    Type: NACA-WR-L-684 , NACA-MR-L5I28a
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  • 71
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    The Knock-Limited Performance of Fuel Blends Containing Spiropentane, Methylenecyclobutane, Di-Tert-Butyl Ether, Methyl Tert-Butyl Ether, and Triptane (1946)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Tests show that at inlet-air temperatures of 250 deg F and 100 deg F the knock-limited performance of the base fuel of blends, leaded with 4 ml TEL per gallon and containing 20 percent spiropentane, was reduced at fuel/air ratios below 0.085. The 20 percent methylenecyclobutane reduced the knock-limited power of the base fuel at fuel/air ratios below 0.112. Di-tert-butyl ether, methyl-tert-butyl ether, and triptane increased the knock-limited power of the base fuel at all fuel/air ratios and at both temperatures.
    Keywords: Aerodynamics
    Type: NACA-WR-E-222 , NACA-RB-E6D22
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  • 72
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    An Investigation of the Ranger V-770-8 Engine Installation for the Edo XOSE-1 Airplane I : Cooling (1945)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Engine temperature data and cooling correlating analyses of the engine and oil cooler are presented in connection with an investigation of the cowling and cooling of the ranger V-770-8 engine installation in the Edo XOSE-1 airplane. Three types of baffles were installed in the course of the tests: the conventional, the turbulent-flow, and the NACA diffuser baffles. Each of the types was of merit in cooling a different region on the cylinder. Incorporation of the best features of the three types into one baffle, a method which appears to be feasible, would provide improvements in cylinder cooling.
    Keywords: Aerodynamics
    Type: NACA-WR-L-561
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  • 73
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    Effects of Compressibility on the Maximum Lift Characteristics and Spanwise Load Distribution of a 12-Foot-Span Fighter-Type Wing of NACA 230-Series Airfoil Sections (1945)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Lift characteristics and pressure distribution for a NACA 230 wing were investigated for an angle of attack range of from -10 to +24 degrees and Mach range of from 0.2 to 0.7. Maximum lift coefficient increased up to a Mach number of 0.3, decreased rapidly to a Mach number of 0.55, and then decreased moderately. At high speeds, maximum lift coefficient was reached at from 10 to 12 degrees beyond the stalling angle. In high-speed stalls, resultant load underwent a moderate shift outward.
    Keywords: Aerodynamics
    Type: NACA-WR-L-51 , NACA-ACR-L5G10
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  • 74
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    Comparison of Pitching Moments Produced by Plain Flaps and by Spoilers and Some Aerodynamic Characteristics of an NACA 23012 Airfoil with Various Types of Aileron (1945)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Sectional characteristics of airfoil having retractable slotted flap with plain, slot-lip, or retractable ailerons are presented for a large range of aileron deflections. The analysis indicated that pitching moments produced by spoilers were less positive than those produced by plain flaps of equal effectiveness, also that pitching moments created by the spoiler increased less with the Mach number than similar moments produced by plain flaps. Positive values of pitching moment decreased as devices were located nearer airfoil leading edge.
    Keywords: Aerodynamics
    Type: NACA-WR-L-124 , NACA-ACR-L5C24a
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  • 75
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    Flight Investigation to Improve the Dynamic Longitudinal Stability and Control-Feel Characteristics of the P-63A-1 Airplane (AAF No. 42-68889) with Closely Balanced Experimental Elevators (1946)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Results of flight tests of a control-feel aid presented. This device consisted of a spring and dashpot connected in series between the control stick and airplane structure. The device was tested in combination with an experimental elevator and bobweight which had given unsatisfactory dynamic stability and control-feel characteristics in previous tests. The control-feel aid effected marked improvement in both the control-feel characteristics and the control-feel dynamic longitudinal stability of the airplane.
    Keywords: Aerodynamics
    Type: NACA-WR-L-730 , NACA-MR-L6E20
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  • 76
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    Elements of the Wing Section Theory and of the Wing Theory (1925)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: This report contains those results of the theory of wings and of wing sections which are of immediate practical value. They are proved and demonstrated by the use of the simple conceptions of "kinetic energy" and "momentum" only, familiar to every engineer; and not by introducing "isogonal transformations" and "vortices," which latter mathematical methods are not essential to the theory and better are used only in papers intended for mathematicians and special experts.
    Keywords: Aerodynamics
    Type: NACA-TR-191
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  • 77
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    Analysis, Verification, and Application of Equations and Procedures for Design of Exhaust-pipe Shrouds (1947)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Investigations were made to develop a simplified method for designing exhaust-pipe shrouds to provide desired or maximum cooling of exhaust installations. Analysis of heat exchange and pressure drop of an adequate exhaust-pipe shroud system requires equations for predicting design temperatures and pressure drop on cooling air side of system. Present experiments derive such equations for usual straight annular exhaust-pipe shroud systems for both parallel flow and counter flow. Equations and methods presented are believed to be applicable under certain conditions to the design of shrouds for tail pipes of jet engines.
    Keywords: Aerodynamics
    Type: NACA-TN-1495
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  • 78
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    Some Recent Contributions to the Study of Transition and Turbulent Boundary Layers (1947)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: The first part of this paper reviews the present state of the problem of the instability of laminar boundary layers which has formed an important part of the general lectures by von Karman at the first and fourth Congresses and by Taylor at the fifth Congress. This problem may now be considered as essentially solved as the result of work completed since 1938. When the velocity fluctuations of the free-stream flow are less than 0.1 percent of the mean speed, instability occurs as described by the well-known Tollmien-Schlichting theory. The Tollmien-Schlichting waves were first observed experimentally by Schubauer and Skramstad in 1940. They devised methods of introducing controlled small disturbances and obtained measured values of frequency, damping, and wave length at various Reynolds numbers which agreed well with the theoretical results. Their experimental results were confirmed by Liepmann. Much theoretical work was done in Germany in extending the Tol1mien-Schlichting theory to other boundary conditions, in particular to flow along a porous wall to which suction is applied for removing part of the boundary layer. The second part of this paper summarizes the present state of knowledge of the mechanics of turbulent boundary layers, and of the methods now being used for fundamental studies of the turbulent fluctuations in turbulent boundary layers. A brief review is given of the semi-empirical method of approach as developed by Buri, Gruschwitz, Fediaevsky, and Kalikhman. In recent years the National Advisory.Commsittee for Aeronautics has sponsored a detailed study at the National Bureau of Standards of the turbulent fluctuations in a turbulent boundary layer under adverse pressure gradient sufficient to produce separation. The aims of this investigation and its present status are described.
    Keywords: Aerodynamics
    Type: NACA-TN-1168
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  • 79
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    Investigation of the Penetration on an Air Jet Directed Perpendicularly to an Air Stream (1948)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: An experimental investigation was conducted to determine the penetration of a circular air Jet directed perpendicularly to an air stream as a function of Jet density, Jet velocity, air-stream density, air-stream velocity, Jet diameter, and distance downstream from the Jet. The penetration was determined for nearly constant values of air-stream density at two tunnel velocities, four Jet diameters, four positions downstream of the Jet, and for a large range of Jet velocities and densities. An equation for the penetration was obtained in terms of the Jet diameter, the distance downstream from the jet, and the ratios of Jet and air-stream velocities and densities.
    Keywords: Aerodynamics
    Type: NACA-TN-1615
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  • 80
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    Field of Flow About a Jet and Effect of Jets on Stability of Jet-Propelled Airplanes (1946)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: A theoretical investigation was conducted on jet-induced flow deviation. Analysis is given of flow inclination induced outside cold and hot jets and jet deflection caused by angle of attack. Applications to computation of effects of jet on longitudinal stability and trim are explained. Effect of jet temperature on flow inclination was found small when thrust coefficient is used as criterion for similitude. The average jet-induced downwash over tail plane was obtained geometrically.
    Keywords: Aerodynamics
    Type: NACA-WR-L-213 , NACA-ACR-L6C13
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  • 81
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    Summary of Airfoil Data (1945)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Recent airfoil data for both flight and wind-tunnel tests have been collected and correlated insofar as possible. The flight data consist largely of drag measurements made by the wake-survey method. Most of the data on airfoil section characteristics were obtained in the Langley two-dimensional low-turbulence pressure tunnel. Detail data necessary for the application of NACA 6-serles airfoils to wing design are presented in supplementary figures, together with recent data for the NACA 24-, 44-, and 230-series airfoils. The general methods used to derive the basic thickness forms for NACA 6- and 7-series airfoils and their corresponding pressure distributions are presented. Data and methods are given for rapidly obtaining the approximate pressure distributions for NACA four-digit, five-digit, 6-, and 7-series airfoils. The report includes an analysis of the lift, drag, pitching-moment, and critical-speed characteristics of the airfoils, together with a discussion of the effects of surface conditions. Available data on high-lift devices are presented. Problems associated with lateral-control devices, leading-edge air intakes, and interference are briefly discussed. The data indicate that the effects of surface condition on the lift and drag characteristics are at least as large as the effects of the airfoil shape and must be considered in airfoil selection and the prediction of wing characteristics. Airfoils permitting extensive laminar flow, such as the NACA 6-series airfoils, have much lower drag coefficients at high speed and cruising lift coefficients than earlier types-of airfoils if, and only if, the wing surfaces are sufficiently smooth and fair. The NACA 6-series airfoils also have favorable critical-speed characteristics and do not appear to present unusual problems associated with the application of high-lift and lateral-control devices. Much of the data given in the NACA Advance Confidential Report entitled "Preliminary Low-Drag-Airfoil and Flap Data from Tests at Large Reynolds Number and Low Turbulence," by Eastman N. Jacobs, Ira R. Abbott, and Milton Davidson, March 1942 has been corrected and included in the present paper, which supersedes the previously published paper.
    Keywords: Aerodynamics
    Type: NACA-ACR-L5005 , NACA-MR-L5I12 , NACA-WR-L-560
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  • 82
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    Statistical Analysis of the Characteristics of Repeated Gusts in Turbulent Air (1945)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Statistical methods were applied to acceleration and airspeed data obtained with the XC-35 airplane during flights in turbulent air within convective clouds in order to determine the characteristics of repeated or closely spaced gusts pertinent to design problems. Results indicated that, in turbulent air within convective cloud, gusts tend to be contiguous and are seldom found isolated in space. Over-all average spacing between repeated gusts was in good agreement with twice the average gust-gradient distance of 10 chords used in present design.
    Keywords: Aerodynamics
    Type: NACA-WR-L-39 , NACA-ARR-L5H30
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  • 83
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    High-Speed Wind-Tunnel Tests of a Twin-Fuselage Pursuit Airplane (1946)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: At the request of the Air Technical Service Command, U.S. Army Air Forces, a 0.22-scale model of a twin-fuselae pursuit airplane was built and tested at the Ames Aeronautical Laboratory. The tests of this model were made in order that the aerodynamic characteristics of the airplane, especially at high speed, might be predicted. The results shown in this report consist of force data for the model and critical Mach numbers of parts of the model as determined from pressure-distribution measurements. The results indicate that a diving tendency of the airplane can be expected at Mach numbers above 0.70 at lift co-efficients from 0 to 0.4. There is an indication that the Mach number at which the airpolane would first experience a diving tendency for lift coefficients from 0 to 0.2 can be increased if the critical speed of the radiator enclosures is increased, and the wing-fuselage-juncture fillets are improved.
    Keywords: Aerodynamics
    Type: NACA-WR-A-75 , NACA-MR-A6D03
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  • 84
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    Completed Tabulation in the United States of Tests of 24 Airfoils at High Mach Numbers (Derived from Interrupted Work at Guidonia, Italy in the 1.31- by 1.74-Foot High-Speed Tunnel) (1945)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Two-dimensional data were obtained in Mach range of from 0.40 to 0.94 and Reynolds Number range of (3.4 - 4.2) X 10 Degrees. Results indicate that thickness ratio is dominating shape parameter at high Mach numbers and that aerodynamic advantages are attainable by using thinnest possible sections. Effects of jet boundaries, Reynolds Number, and Data presented are free from jet-boundary and humidity effects.
    Keywords: Aerodynamics
    Type: NACA-WR-L-143 , NACA-ACR-L5E21
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  • 85
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    Flight Investigation at High Speeds of Profile Drag of Wing of a P-47D Airplane Having Production Surfaces Covered with Camouflage Paint (1946)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Wing section outboard of flap was tested by wake surveys in Mach range of 0.25 - 0.78 and lift coefficient range 0.06 - 0.69. Results indicated that minimum profile-drag coefficient of 0.0097 was attained for lift coefficients from 0.16 to 0.25 at Mach less than 0.67. Below Mach number at which compressibility shock occurred, variations in Mach of 0.2 had negligible effect on profile drag coefficient. Shock was not evident until critical Mach was exceeded by 0.025.
    Keywords: Aerodynamics
    Type: NACA-WR-L-98 , NACA-ACR-L6B21
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  • 86
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    Comparison of Wind-Tunnel and Flight Measurements of Stability and Control Characteristics of a Douglas A-26 Airplane (1946)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Tests in Langley pressure tunnel of model XA-26 bomber were compared with those of A-26B (twin-engine attack bomber) and showed that static longitudinal stability, indicated by elevator-fixed neutral points, and variation of elevator deflection in straight and turning flight were good. Airplane possessed improved stability at low speeds which was attributed to pronounced stalling at root of production wing. At rudder-force reversal at speeds higher than those in flight tests, agreement in rudder-fixed and rudder-free static directional stability was good. Hinge moment obtained at zero sideslip was satisfactory for determining aileron forces in sideslip.
    Keywords: Aerodynamics
    Type: NACA-WR-L-99 , NACA-ARR-L5H11a
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  • 87
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    Flow and Drag Formulas for Simple Quadrics (1927)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: This report gives the pressure distribution and resistance found by theory and experiment for simple quadrics fixed in an infinite uniform stream of practically incompressible fluid. The experimental values pertain to air and some liquids, especially water; the theoretical refer sometimes to perfect, again to viscid fluids. For the cases treated the concordance of theory and measurement is so close as to make a resume of results desirable. Incidentally formulas for the velocity at all points of the flow field are given, some being new forms for ready use derived in a previous paper. (author)
    Keywords: Aerodynamics
    Type: NACA-TR-253
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  • 88
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    Wind-tunnel Tests of the 0.15-scale Powered Model of the Fleetwings XBTK-1 Airplane : Longitudinal Stability and Control (1945)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: An investigation was made of the static longitudinal stability, and control and stall characteristics of XBTK-1 dive bomber. Results indicate that the longitudinal stability will probably be satisfactory for all contemplated flight conditions at the rear-most CG location with elevator both fixed and free. Power effects were small. Sufficient elevator control will be available to trim in any flight condition above the ground. Increasing the slotted flap deflection above 30 degrees only slightly increased the max. lift coefficient.
    Keywords: Aerodynamics
    Type: NACA-WR-L-785 , NACA-MR-L5D27a
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  • 89
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    Analysis of V-G Records from the SNB-1 Airplane (1946)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Availability data obtained on SNB-1 trainer-class airplanes were analyzed and results presented as flight envelopes which predict occurrences of large values of air speed and acceleration. Comparison is made with SNJ-4 trainer-class airplane data analyzed by the same method. It is concluded that flight envelopes are satisfactory; that the two types show large differences in flight loads and speeds experience; and that SNB-1 will seldom, if ever, exceed design limit load factor and restricted speed, which SNJ-4 can be expected to exceed design-limit load factor and restricted speed in a very small number of flight hours.
    Keywords: Aerodynamics
    Type: NACA-WR-L-759 , NACA-MR-L6F27a
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  • 90
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    Measurement of Flying Qualities of a Dehavilland Mosquito F-8 Airplane (AAF No. 43-334960) I: Lateral and Directional Stability and Control Characteristics (1945)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: The data presented have no bearing on performance characteristics of airplane, which were considered exceptionally good in previous tests. Some of the undesirable features of lateral and directional stability and control characteristics of the F-8 are listed. Directional stability, with rudder fixed, did not sufficiently restrict aileron yaw; rudder control was inadequate during take-off and landing, and was insufficient to fly airplane with one engine; in clean condition, power of ailerons was slightly below minimum value specified; it was difficult to trim airplane in rough air.
    Keywords: Aerodynamics
    Type: NACA-WR-L-593 , NACA-MR-L5D19
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  • 91
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    The Knock-Limited Performance of Fuel Blends Containing Aromatics V : N-Propylbenzene, N-Butylbenzene, Isobutylbenzene, M-Xylene, and 1-Isopropyl-4-Methylbenzene (1946)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Results are reported of knock-limited tests of five aromatics, each individually blended with selected base fuels and tested with and without TEL, using 17.6, F-4, and F-3 small-scale engines. The five aromatics rated in the following order of decreasing antiknock effectiveness at fuel/air ratio 0.10: m-xylene, 1-isopropyl-4-methylbenzene, n-propylbenzene, isobutylbenzene, and n-butylbenzene.
    Keywords: Aerodynamics
    Type: NACA-WR-E-237 , NACA-ARR-E6C05
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  • 92
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    An Experimental Investigation of Flow Conditions in the Vicinity of an NACA D(sub S)-type Cowling (1946)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Data are presented of the flow conditions in the vicinity of an NACA D sub S -type cowling. Tests were made of a 1/2 scale-nacelle model at inlet-velocity ratios ranging from 0.23 to 1.02 and angles of attack from 6 deg to 10 deg. The velocity and direction of flow in the vertical plane of symmetry of the cowling were determined from orifices and tufts installed on a board aligned with the flow. Diagrams showing velocity ratio contours and lines of constant flow angles are given.
    Keywords: Aerodynamics
    Type: NACA-WR-L-747 , NACA-MR-L6H14
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  • 93
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    Flight Investigation of Boundary-layer and Profile-drag Characteristics of Smooth Wing Sections of a P-47D Airplane (1945)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: In Mach range of 0.25 - 0.69, boundary-layer measurements were made on upper wing surface at 25% semi-span, pressure-distribution measurements made on upper surface at 63% semi-span, and wake surveys made at 63% semi-span. The minimum profile-drag coefficient of 0.0062 was indicated for smooth section at 63% semi-span. Critical mach number was exceeded by 0.04, but no compressibility shocks appeared. In slipstream, boundary layer transition occurred as far back as 20% chord on upper surface at low lift coefficients.
    Keywords: Aerodynamics
    Type: NACA-WR-L-86 , NACA-ARR-L5H11A
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  • 94
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    Development of Wing Inlets (1946)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Lift, drag, internal flow, and pressure distribution measurements were made on a low-drag airfoil incorporating various air inlet designs. Two leading-edge air inlets are developed which feature higher lift coefficients and critical Mach than the basic airfoil. Higher lift coefficients and critical speeds are obtained for leading half of these inlet sections but because of high suction pressures near exist, slightly lower critical speeds are obtained for the entire inlet section than the basic airfoil.
    Keywords: Aerodynamics
    Type: NACA-WR-L-727 , NACA-ACR-L6B18
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 95
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    Flight Tests of the Lateral Control Characteristics of an F6F-3 Airplane Equipped with Spring-Tab Ailerons (1945)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Tests were made to determine whether spring-tab ailerons tended to oscillate or flutter in speed ranges up to 400 mph. Flight tests showed spring-tab ailerons had desirable light stick forces and no tendency to overbalance. No flutter tendencies were indicated up to 400 mph, and any oscillations following abrupt control deflections were heavily damped. Recommendations were made for modifications to increase aileron effectiveness at low speeds without affecting lateral control at high speeds by increasing available deflection and modifying spring-tab arrangement.
    Keywords: Aerodynamics
    Type: NACA-WR-L-149 , NACA-ARR-L5C23
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 96
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    Critical Mach Numbers of Thin Airfoil Sections with Plain Flaps (1946)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Critical Mach number as function of lift coefficient is determined for certain moderately thick NACA low-drag airfoils. Results, given graphically, included calculations on same airfoil sections with plain flaps for small flap deflections. Curves indicate optimum critical conditions for airfoils with flaps in such form that they can be compared with corresponding results for zero flap deflections. Plain flaps increase life-coefficient range for which critical Mach number is in region of high values characteristic of low-drag airfoils.
    Keywords: Aerodynamics
    Type: NACA-WR-W-2 , NACA-ACR-6A30
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 97
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    Determination of the Stability and Control Characteristics of a Tailless All-Wing Airplane Model with Sweepback in the Langley Free-Flight Tunnel (1945)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Force and flight tests were performance on an all-wing model with windmilling propellers. Tests were conducted with deflected and retracted flaps, with and without auxiliary vertical tail surfaces, and with different centers of gravity and trim coefficients. Results indicate serious reduction of stick-fixed longitudinal stability because of wing-tip stalling at high lift coefficient. Directional stability without vertical tail is undesirably low. Low effective dihedral should be maintained. Elevator and rudder control system is satisfactory.
    Keywords: Aerodynamics
    Type: NACA-WR-L-50 , NACA-ACR-L5A13
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 98
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    Tests of Four Full-scale Propellers to Determine the Effect of Trailing-edge Extensions on Propeller Aerodynamic Characteristics (1945)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Propellers with trailing-edge extensions were studied to determine aerodynamic characteristics. Trailing-edge extension increased power absorbed by propeller with little loss in efficiency. Power coefficient for maximum efficiency was greater for 20% camber type extension than for 20% straight type extension over range of advance ratio of 1.0 to 2.5 although camber type was less efficient. Efficiency was about the same for cruising and high-speed at a high power coefficient for propeller with extension.
    Keywords: Aerodynamics
    Type: NACA-WR-L-582
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 99
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    An Investigation of the Ranger V-770-8 Engine Installation for the Edo XOSE-1 Airplane II : Aerodynamics (1945)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Investigations were made to determine the cowling and cooling characteristics of the Ranger V-770-8 engine installation in an observation seaplane. Final cowl configurations possessed ample engine and oil-cooler pressure drops for cooling in the critical normal-power climb condition with any of the three baffle configurations tested. The indicated critical Mach number of the cowling was found to be 0.70 as determined by the pressure on the lower lip of the inlet.
    Keywords: Aerodynamics
    Type: NACA-WR-L-562 , NACA-MR-L5I12b
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 100
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    Analysis of Effect of Rolling Pull-Outs on Wing and Aileron Loads of a Fighter Airplane (1946)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: An analysis was made to determine the effect of rolling pull-out maneuvers on the wing and aileron loads of a typical fighter airplane, the P-47B. The results obtained indicate that higher loads are imposed upon wings and ailerons because of the rolling pull-out maneuver, than would be obtained by application of the loading requirements to which the airplane was designed. An increase of 102 lb or 15 percent of wing weight would be required if the wing were designed for rolling pull-out maneuver. It was also determined that the requirements by which the aileron was originally designed were inadequate.
    Keywords: Aerodynamics
    Type: NACA-WR-L-270
    Format: application/pdf
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    NASA TECHNICAL REPORTS
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