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  • Fluid Mechanics and Thermodynamics
  • Temperatur
  • unknown
  • 1990-1994  (113)
  • 1945-1949  (112)
  • 1
    ISSN: 0009-286X
    Keywords: Schüttgut ; EVA-Copolymer ; Lagerung ; Silo ; Fließeigenschaft ; Zeitverfestigung ; Temperatur ; Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
    Additional Material: 4 Ill.
    Type of Medium: Electronic Resource
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  • 2
    Electronic Resource
    Electronic Resource
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 64 (1992), S. 210-211 
    ISSN: 0009-286X
    Keywords: Hochdruck ; Messung ; Volumen ; Druck ; Temperatur ; Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
    Additional Material: 2 Ill.
    Type of Medium: Electronic Resource
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  • 3
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    In:  Zeitschrift für Pflanzenernährung, Düngung, Bodenkunde 46:176-190
    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
    Publication Date: 1949
    Description: Der Autor untersuchte im Freiland die Zeiten zu denen Ausschlüpfen, Begattung und Eiablage des Springwurmwicklers stattfindet. Zudem wurden Temperatur und relative Luftfeuchte gemessen und mit den Beobachtungen zum Schaderreger in Verbindung gesetzt. KATASTER-BESCHREIBUNG: KATASTER-DETAIL:
    Keywords: Breisgau, Freiburg ; 1943-1944 ; Luftfeuchte ; Pflanzenschädling ; Temperatur ; Wein
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  • 5
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    In:  Nachrichten Blatt für den deutschen Pflanzenschutzdienst, p. 101-104
    Publication Date: 1947
    Description: Beobachtungen zu den Witterungsverhältnissen im Winter 1946/47 und im Sommer 1947 und deren Auswirkungen auf den Rapserdfloh sowie ein Vergleich mit ähnlichen vergangenen Ereignissen KATASTER-BESCHREIBUNG: Zusammenhang zwischen Witterung (Temperatur und Niederschlag) und der Entwicklung des Rapserdflohs KATASTER-DETAIL: Delta T: T 〈 6°C, dann Eiablage; Delta T +, dann Schlüpfergebnis -; T 〉 30°C, dann keine Entwicklung von Larven Delta Nied -, dann Austrocknung der Eier +;
    Keywords: Mecklenburg, Thüringen, Sachsen, Brandenburg ; 1946-1947 ; Boden ; Niederschlag ; Pflanzenschädling ; Temperatur ; Trockenheit ; Witterung ; Raps
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  • 6
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    In:  Zeitschrift für Pflanzenernährung, Düngung, Bodenkunde 40:114-129.
    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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  • 7
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    In:  Verh. Schweiz. Naturforsch. Ges. Freiburg, 135-137
    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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  • 8
    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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  • 9
    Publication Date: 1947
    Description: Untersuchungen zur Entwicklung der Obstbaumspinnmilbe, ihrer Eiablage und ihres sonstigen Verhaltens unter natürlichen Umweltbedingungen KATASTER-BESCHREIBUNG: Zusammenhänge zwischen Temperatur und Niederschlag und der Anzahl und dem zeitlichen Vorkommen der Generationen sowie des Schlüpfens der Larven. KATASTER-DETAIL: Delta Nied +, dann Zeit für Entwicklung der Milben +; Delta T +, dann Zeit von Eiablage bis Schlüpfen -; Delta T + ,Delta Sonn + und/oder Delta Relf +, dann Anzahl schlüpfender Larven +; Delta T - und/oder Delta Nied +, dann Zeit für Entwicklung der Larven und Nymphen +; Delta T - und/oder Delta Nied +, dann Mortalität(Larven und Nymphen)+; Delta T + und Delta Relf -, dann Anzahl gelegter Sommereier +; Delta T +, dann Zeit für Entwicklung der Sommereier -; Delta T -, dann Anzahl gelegter Wintereier -; T 〈= 8°C, dann keine Eiablage; Delta Wind +, dann Anzahl abgewehter Milben +; Delta T (Frühjahr und Sommer) + und Delta Relf (Frühjahr und Sommer) -, dann starker Befall
    Keywords: Bergisches Land und Labor ; 1943-1944, 1946 ; Niederschlag ; Pflanzenschädling ; Temperatur ; Witterung ; Obst
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  • 10
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    In:  Nachr. Bl. Biolog. Ztr.-Anst. Braunschweig, p.19
    Publication Date: 1949
    Description: Verbale Beschreibung des Massenauftretens 1948 sowie früheren Massenauftretens (1891, 1922, 1925, 1938 und 1939) KATASTER-BESCHREIBUNG: Zusammenhang zwischen Witterung (Temperatur und Luftfeuchte) und dem Massenauftreten des Käfers KATASTER-DETAIL: Delta T + (Sommer und Winter) und Delta Relf (Sommer) -, dann Massenauftreten im Folgejahr
    Keywords: Deutschland ; 1947-1948 ; Zuckerrüben ; Pflanzenschädling ; Temperatur ; Trockenheit ; Witterung ; Gemüse
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  • 11
    Publication Date: 1948
    Description: Allgemeine Beobachtungen zur Lebensweise des Rüben-Derbrüsslers KATASTER-BESCHREIBUNG: Zusammenhang zwischen dem Massenauftreten des Käfers und der Witterung im Frühjahr und Sommer KATASTER-DETAIL: Delta T: T 〈 12-14°C, dann Ende der Winterruhe; Delta T+, dann Flugbeginn; Delta Nied (Frühjahr und Sommer) +, dann Massenauftreten +;
    Keywords: Sachsen-Anhalt ; 1948 ; Zuckerrüben ; Niederschlag ; Pflanzenschädling ; Temperatur ; Trockenheit ; Witterung
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  • 12
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    In:  Nachr. Bl. Deutscher Pflanzenschutzdienst, p. 133
    Publication Date: 1948
    Description: Verbale Beschreibung zur Verbeitung und zum Jahreszyklus des Rüben-Derbrüsslers KATASTER-BESCHREIBUNG: Zusammenhang zwischen Temperatur und Jahreszyklus des Käfers KATASTER-DETAIL: Delta T: T (Luft)〉 12-14°C, dann Ende der Winterruhe
    Keywords: Deutschland ; 1946-48 ; Zuckerrüben ; Pflanzenschädling ; Temperatur
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  • 13
    Publication Date: 1948
    Description: Untersuchungen zu den klimatischen Bedingungen, welche im Freiland den Befall der Gurkenfrüchte mit dem Erreger der Krätze begünstigen KATASTER-BESCHREIBUNG: Zusammenhang zwischen dem Krätzebefall und der Luftfeuchte sowie der Temperatur KATASTER-DETAIL: Relf -, dann Infektionserfolg -; Relf〉90% (bei t〉4h), dann Infektionserfolg; T〈20°C, dann Infektionserfolg -
    Keywords: Sachsen-Anhalt ; 1947 ; Luftfeuchte ; Pflanzenkrankheit ; Temperatur ; Witterung ; Gemüse
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  • 14
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    In:  Z. Pflanzenkrankheiten (Pflanzenpathol.) Pflanzenschutz, Nov./Dez., p. 335-341,
    Publication Date: 1948
    Description: Bericht über allgemeine Beobachtungen zum Flug und zu den Wandergewohnheiten des Großen Kohlweißlings KATASTER-BESCHREIBUNG: Einfluss von Wind und Sonnenscheindauer auf den Flug des Kohlweißlings KATASTER-DETAIL: Wind 〉 20km/h, dann kein Flug; Delta Sonn +, dann Flug +;
    Keywords: Deutschland ; 1942-48 ; Pflanzenschädling ; Temperatur ; Sonnenscheindauer ; Kohl
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  • 15
    Publication Date: 1949
    Description: Bericht über die Untersuchungen der mikroklimatischen Temperatur- und Feuchtigkeitsbedingungen in Ackerbohnenbeständen sowie über die Beobachtungen des biogenen Vorganges KATASTER-BESCHREIBUNG: Zusammenhang zwischen der Witterung (Temperatur und Luftfeuchte) und der Stärke des Sporenaustritts KATASTER-DETAIL: Delta T und Delta Relf: 8°C 〈 T 〈 22°c und t (Relf 〉 90%) 〉 8h, dann Sporenaustritt ++; t (Benetzung mit tropfbar flüssigem Wasser) +, dann Sporenaustritt +
    Keywords: Sachsen-Anhalt ; 1948 ; Luftfeuchte ; Pflanzenkrankheit ; Temperatur ; Witterung ; Benetzung ; Gemüse
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  • 16
    Publication Date: 1948
    Description: Bericht über die Laboruntersuchungen von Raps- und Rübsenproben auf den Befall mit Rapserdflohlarven KATASTER-BESCHREIBUNG: Einfluss von Temperatur und Trockenheit auf die Entwicklung des Rapserdflohs KATASTER-DETAIL: Delta T + und Delta Nied -, dann spätere Eiablage; Delta Nied -, dann Entwicklung der Eier -
    Keywords: Mecklenburg, Thüringen, Sachsen, Brandenburg ; 1947-1948 ; Luftfeuchte ; Pflanzenschädling ; Temperatur ; Raps
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  • 17
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    In:  Annalen der Meteorologie, S. 326-328.
    Publication Date: 1948
    Description: Entwicklung eines "Wetterschadensfaktor", der Zusammenhang zwischen Witterung und Ernteertrag beschreibt KATASTER-BESCHREIBUNG: - KATASTER-DETAIL: -
    Keywords: Schleswig-Holstein ; 1933-42 ; Kartoffeln ; Ertrag ; Korrelationsmethode ; Landwirtschaft ; Niederschlag ; Temperatur ; Witterung
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  • 18
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    In:  Nachrichtenblatt für den Deutschen Pflanzenschutzdienst, Heft 7/8, p.105-112
    Publication Date: 1948
    Description: Untersuchungen im Berliner Botanischen Garten, im Institut für Züchtungsforschungen in Müncheberg/Mark und im Obstbezirk des Alten Landes bei Hamburg/Stade über das Auftreten von Larven, die aus überwinterten Eiern auf Obstbäumen geschlüpft sind sowie Untersuchungen zur Temperaturempfindlichkeit der Fundatrix-Larven und der Sommerform von Myzodes Persicae im Labor. KATASTER-BESCHREIBUNG: Zusammenhang ziwschen Temperatur, Niederschlag sowie relativer Luftfeuchte und dem Überwinterungserfolg KATASTER-DETAIL: Delta T -, Delta Nied ++, Delta Relf +, dann Myzodes persicae -; T 〈 -9°C, dann Myzodes persicae -; T 〈 -12°C (d 〉 1), dann Tod
    Keywords: Deutschland, Labor ; 1933 - 1948 ; Niederschlag ; Pflanzenschädling ; Temperatur
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  • 19
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    In:  Zeitschr. Pflanzenernährung, Düngung, Bodenkunde 40: 114-129
    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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  • 20
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    In:  CASI
    Publication Date: 2006-10-26
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    Publication Date: 2005-11-02
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  • 55
    Publication Date: 2011-08-23
    Description: The effect of rapid mean compression on compressible turbulence at a range of turbulent Mach numbers is investigated. Rapid dist'ortion theory (RDT) and direct numerical simulation results for the case of axial (one-dimensional) compression are used to illustrate the existence of two distinct rapid compression regimes. These regimes - the nearly solenoidal and the 'pressure-released' - are defined by a single parameter involving the timescales of the mean distortion, the turbulence, and the speed of sound. A general RDT formulation is developed and is proposed as a means of improving turbulence models for compressible flows. In contrast to the well-documented observation that 'compressibility' (measured, for example, by the turbulent Mach number) is often associated with a decrease in the growth rate of turbulent kinetic energy, we find that under rapid distortion compressibility can produce an amplification of the kinetic energy growth rate. We also find that as the compressibility increases, the magnitude of the pressure-dilation correlation increases, in absolute terms, but its relative importance decreases compared to the magnitude of the kinetic energy production.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Journal of Fluid Mechanics; Volume 257; 641-665
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  • 56
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    In:  CASI
    Publication Date: 2018-06-09
    Description: Developed under a Small Business Innovation Research (SBIR) contract, RAMPANT is a CFD software package for computing flow around complex shapes. The package is flexible, fast and easy to use. It has found a great number of applications, including computation of air flow around a Nordic ski jumper, prediction of flow over an airfoil and computation of the external aerodynamics of motor vehicles.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Spinoff 1993; 90-91; NASA-NP-211
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  • 57
    Publication Date: 2018-06-12
    Description: A dual-frequency acoustic levitator containing water was developed for studying bubble and drop dynamics in low gravity. It was flown on USML-1 where it was used in the Glovebox facility. High frequency (21 or 63 kHz) ultrasonic waves were modulated by low frequencies to excite shape oscillations on bubbles and oil drops ultrasonically trapped in the water. Bubble diameters were typically close to 1 cm or larger. When such large bubbles are acoustically trapped on the Earth, the acoustic radiation pressure needed to overcome buoyancy tends to shift the natural frequency for quadrupole (n = 2) oscillations above the prediction of Lamb's equation. In low gravity, a much weaker trapping force was used and measurements of n = 2 and 3 mode frequencies were closer to the ideal case. Other video observations in low gravity include: (i) the transient reappearance of a bulge where a small bubble has coalesced with a large one, (ii) observations of the dynamics of bubbles coated by oil indicating that shape oscillations can shift a coated bubble away from the oil-water interface of the coating giving a centering of the core, and (iii) the agglomeration of bubbles induced by the sound field.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Joint Launch + One Year Science Review of USML-1 and USMP-1 with the Microgravity Measurement Group, Volume 2; 673-690; NASA-CP-3272-Vol-2
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  • 58
    Publication Date: 2018-06-05
    Description: A study of instabilities in incompressible boundary-layer flow on a flat plate is conducted by spatial direct numerical simulation (DNS) of the Navier-Stokes equations. Here, the DNS results are used to critically evaluate the results obtained using parabolized stability equations (PSE) theory and to study mechanisms associated with breakdown from laminar to turbulent flow. Three test cases are considered: two-dimensional Tollmien-Schlichting wave propagation, subharmonic instability breakdown, and oblique-wave break-down. The instability modes predicted by PSE theory are in good quantitative agreement with the DNS results, except a small discrepancy is evident in the mean-flow distortion component of the 2-D test problem. This discrepancy is attributed to far-field boundary- condition differences. Both DNS and PSE theory results show several modal discrepancies when compared with the experiments of subharmonic breakdown. Computations that allow for a small adverse pressure gradient in the basic flow and a variation of the disturbance frequency result in better agreement with the experiments.
    Keywords: Fluid Mechanics and Thermodynamics
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  • 59
    Publication Date: 2018-06-05
    Description: A new measurement technique is being developed by NASA to measure off-surface flow fields. This method, Doppler global velocimetry, will allow quantification of complex three-dimensional flow fields at video camera rates. The entire flow field structure within a selected plane is measured simultaneously rather than by scanned, point-by-point measurements using conventional laser velocimetry. Data obtained using this technique will be used to correlate with other data sets for verification, and following verification, provide a quantified, highly detailed definition of the flow field. This will help to improve the understanding of fluid physics, supplement and broaden the database required to validate and refine computational fluid dynamics (CFD) models, and improve aircraft design methodology. To assess the capability of the technique, velocity measurements of the vortical flow field above a thin 75-degree delta wing were made in the NASA - Langley Basic Aerodynamics Research Tunnel. Preliminary comparisons of the results were made with similar measurements obtained using a three component laser velocimeter indicate that this technique is capable of describing the entire three - component velocity flow field simultaneously within a measurement plane in real time.
    Keywords: Fluid Mechanics and Thermodynamics
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  • 60
    Publication Date: 2018-06-05
    Description: The spatial evolution of cross flow-vortex packets in a laminar boundary layer on a swept wing are computed by the direct numerical simulation of the incompressible Navier- Stokes equations. A wall-normal velocity distribution of steady suction and blowing at the wing surface is used to generate a strip of equally spaced and periodic disturbances along the span. Three simulations are conducted to study the effect of initial amplitude on the disturbance evolution, to determine the role of traveling cross ow modes in transition, and to devise a correlation function to guide theories of transition prediction. In each simulation, the vortex packets first enter a chordwise region of linear independent growth, then, the individual packets coalesce downstream and interact with adjacent packets, and, finally, the vortex packets nonlinearly interact to generate inflectional velocity profiles. As the initial amplitude of the disturbance is increased, the length of the evolution to breakdown decreases. For this pressure gradient, stationary modes dominate the disturbance evolution. A two-coeffcient function was devised to correlate the simulation results. The coefficients, combined with a single simulation result, provide sufficient information to generate the evolution pattern for disturbances of any initial amplitude.
    Keywords: Fluid Mechanics and Thermodynamics
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  • 61
    Publication Date: 2018-06-02
    Description: A new nonintrusive flow diagnostics instrumentation system, Doppler global velocimetry, is presented. The system is capable of making simultaneous, three-component velocity measurements within a selected measurement plane at video camera rates. These velocity images can provide the researcher with spatial and temporal information about the flow field in a global sense. The investigation of a vortical flow above a 75-degree delta wing comparing standard three-component, fringe-type laser velocimetry measurements with Doppler global velocimetry measurements is presented.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Journal of Aerospace Engineering; Volume 208; Part G; 99-105
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  • 62
    Publication Date: 2019-05-31
    Keywords: unknown
    Type: PR-1-46
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  • 63
    facet.materialart.
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    In:  CASI
    Publication Date: 2019-05-31
    Keywords: unknown
    Type: JPL-PR-4-97
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  • 64
    Publication Date: 2019-05-31
    Keywords: unknown
    Type: JPL-PR-4-94
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  • 65
    Publication Date: 2019-05-25
    Keywords: unknown
    Type: JPL-MEMO-9-16 , AD-96041
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  • 66
    Publication Date: 2019-05-25
    Keywords: unknown
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  • 67
    Publication Date: 2019-05-25
    Keywords: unknown
    Type: NACA-TN-1070
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  • 68
    Publication Date: 2019-05-25
    Keywords: unknown
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  • 69
    Publication Date: 2019-05-25
    Keywords: unknown
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  • 70
    Publication Date: 2018-06-02
    Description: This paper documents the development of the National Aeronautics and Space Administration s (NASA) Langley Research Center ( LaRC) Coherent Antistokes Raman Spectroscopy (CARS) systems for measurements of temperature in a turbulent subsonic or supersonic reacting hydrogen-air environment. Spectra data provides temperature data when compared to a precalculated library of nitrogen CARS spectra. Library validity was confirmed by comparing CARS temperatures derived through the library with three different techniques for determination of the temperature in hydrogen-air combustion and an electrically heated furnace. The CARS system has been used to survey temperature profiles in the simulated flow of a supersonic combustion ramjet (scramjet) model. Measurement results will be discussed.
    Keywords: Fluid Mechanics and Thermodynamics
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  • 71
    Publication Date: 2018-06-02
    Description: An implicit, Navier-Stokes solution algorithm is presented for the computation of turbulent flow on unstructured grids. The inviscid fluxes are computed using an upwind algorithm and the solution is advanced in time using a backward-Euler time-stepping scheme. At each time step, the linear system of equations is approximately solved with a point-implicit relaxation scheme. This methodology provides a viable and robust algorithm for computing turbulent flows on unstructured meshes. Results are shown for subsonic flow over a NACA 0012 airfoil and for transonic flow over a RAE 2822 airfoil exhibiting a strong upper-surface shock. In addition, results are shown for 3 element and 4 element airfoil configurations. For the calculations, two one equation turbulence models are utilized. For the NACA 0012 airfoil, a pressure distribution and force data are compared with other computational results as well as with experiment. Comparisons of computed pressure distributions and velocity profiles with experimental data are shown for the RAE airfoil and for the 3 element configuration. For the 4 element case, comparisons of surface pressure distributions with experiment are made. In general, the agreement between the computations and the experiment is good.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Computers Fluids; Volume 23; No. 1; 1-21
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  • 72
    facet.materialart.
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    In:  CASI
    Publication Date: 2018-06-02
    Description: A technique is presented for triangulation of NURBS surfaces. This technique is built upon an advancing front technique combined with grid point projection. This combined approach has been successfully implemented for structured and unstructured grids.
    Keywords: Fluid Mechanics and Thermodynamics
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  • 73
    Publication Date: 2019-05-31
    Keywords: unknown
    Type: JPL-EP-126
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  • 74
    Publication Date: 2019-05-22
    Keywords: unknown
    Type: REPT.-872
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  • 75
    Publication Date: 2019-05-22
    Keywords: unknown
    Type: JPL-MEMO-9-6
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  • 76
    Publication Date: 2019-05-22
    Keywords: unknown
    Type: MEMO. 4-8
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  • 77
    Publication Date: 2018-06-12
    Description: An experiment was performed on oscillatory thermocapillary flow in the Glovebox aboard the USML-1 Spacelab which was launched in July, 1992. Cylindrical containers of 1 and 3 em in diameter were used. Silicone oils of 2 and 5 cSt viscosity were the test fluids. The fluid was heated by a cylindrical heater placed along the centerline of the container. The diameter of the heater was 10% of the container diameter. The fluid motion was studied by flow visualization. Although oscillations were observed briefly, bubbles generated in the fluid during the experiment disturbed the flow substantially so that the critical temperature differences could not be determined.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Joint Launch + One Year Science Review of USML-1 and USMP-1 with the Microgravity Measurement Group, Volume 2; 701-715; NASA-CP-3272-Vol-2
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  • 78
    Publication Date: 2019-06-27
    Keywords: unknown
    Type: NACA-RM-SL9F23
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  • 79
    Publication Date: 2019-07-18
    Description: The field of Computational Fluid Dynamics (CFD) has advanced to the point where it can now be used for many applications in fluid mechanics research and aerospace vehicle design. A few applications being explored at NASA Ames Research Center will be presented and discussed. The examples presented will range in speed from hypersonic to low speed incompressible flow applications. Most of the results will be from numerical solutions of the Navier-Stokes or Euler equations in three space dimensions for general geometry applications. Computational results will be used to highlight the presentation as appropriate. Advances in computational facilities including those associated with NASA's CAS (Computational Aerosciences) Project of the Federal HPCC (High Performance Computing and Communications) Program will be discussed. Finally, opportunities for future research will be presented and discussed. All material will be taken from non-sensitive, previously-published and widely-disseminated work.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Oct 28, 1994; AZ; United States
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  • 80
    Publication Date: 2019-07-18
    Description: Line Integral Convolution (LIC) is a powerful technique for imaging and animating vector fields. We extend the LIC paradigm in three ways: (1) The existing technique is limited to vector fields over a regular Cartesian grid. We extend it to vector fields over parametric surfaces, such as those found in curvilinear grids, used in computational fluid dynamics simulations; (2) Periodic motion filters can be used to animate the flow visualization. When the flow lies on a parametric surface, however, the motion appears misleading. We explain why this problem arises and show how to adjust the LIC algorithm to handle it; (3) We introduce a technique to visualize vector magnitudes as well as vector direction. Cabral and Leedom have suggested a method for variable-speed animation, which is based on varying the frequency of the filter function. We develop a different technique based on kernel phase shifts which we have found to show substantially better results. Our implementation of these algorithms utilizes texture-mapping hardware to run in real time, which allows them to be included in interactive applications.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Visualization 1994; Oct 17, 1994 - Oct 21, 1994; Washington, DC; United States
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  • 81
    Publication Date: 2019-07-18
    Description: The proposed paper will present a numerical investigation of the flow characteristics and boundary layer development in the nozzles of high enthalpy shock tunnel facilities used for hypersonic propulsion testing. The computed flow will be validated against existing experimental data. Pitot pressure data obtained at the entrance of the test cabin will be used to validate the numerical simulations. It is necessary to accurately model the facility nozzles in order to characterize the test article flow conditions. Initially the axisymmetric nozzle flow will be computed using a Navier Stokes solver for a range of reservoir conditions. The calculated solutions will be compared and calibrated against available experimental data from the DLR HEG piston-driven shock tunnel and the 16-inch shock tunnel at NASA Ames Research Center. The Reynolds number is assumed to be high enough at the throat that the boundary layer flow is assumed turbulent at this point downstream. The real gas affects will be examined. In high Mach number facilities the boundary layer is thick. Attempts will be made to correlate the boundary layer displacement thickness. The displacement thickness correlation will be used to calibrate the quasi-1D codes NENZF and LSENS in order to provide fast and efficient tools of characterizing the facility nozzles. The calibrated quasi-1D codes will be implemented to study the effects of chemistry and the flow condition variations at the test section due to small variations in the driver gas conditions.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: 29th AIAA Thermophysics Conference; Jun 19, 1995 - Jun 22, 1995; San Diego, CA; United States
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  • 82
    Publication Date: 2019-07-18
    Description: In a numerical flow simulation. it is common to generate several thousand time steps of unsteady (time-dependent) flow data. Each time step may require tens to hundreds of megabytes for disk storage, and the total disk requirement for storing the unsteady flow data may be hundreds of gigabytes. Interactive visualization of unsteady flow data of this magnitude is presently impossible with the current hardware technology. This chapter describes the current approaches for unsteady flow visualization. An effective particle tracing technique for unsteady flow is also described. First, the life cycle of a typical numerical flow simulation is outlined. Several unsteady flow data sets from real-world problems are then given. The current approaches for visualizing unsteady flow are then described. There are many existing systems for flow visualization, and some of them are discussed. Streaklines depict time-varying phenomena that are sometimes difficult or impossible to see with other visualization techniques. The algorithms for computing streaklines are described. Several unsteady flow data sets have been visualized using streaklines, and the results are presented. Finally, some current issues in unsteady flow visualization are discussed.
    Keywords: Fluid Mechanics and Thermodynamics
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  • 83
    Publication Date: 2019-07-17
    Description: We have implemented a three-dimensional compressible Navier-Stokes code on the Connection Machine CM-5. The code is set up for implicit time-stepping on single or multiple structured grids. For multiple grids and geometrically complex problems, we follow the 'chimera' approach, where flow data on one zone is interpolated onto another in the region of overlap. We will describe our design philosophy and give some timing results for the current code. A parallel machine like the CM-5 is well-suited for finite-difference methods on structured grids. The regular pattern of connections of a structured mesh maps well onto the architecture of the machine. So the first design choice, finite differences on a structured mesh, is natural. We use centered differences in space, with added artificial dissipation terms. When numerically solving the Navier-Stokes equations, there are liable to be some mesh cells near a solid body that are small in at least one direction. This mesh cell geometry can impose a very severe CFL (Courant-Friedrichs-Lewy) condition on the time step for explicit time-stepping methods. Thus, though explicit time-stepping is well-suited to the architecture of the machine, we have adopted implicit time-stepping. We have further taken the approximate factorization approach. This creates the need to solve large banded linear systems and creates the first possible barrier to an efficient algorithm. To overcome this first possible barrier we have considered two options. The first is just to solve the banded linear systems with data spread over the whole machine, using whatever fast method is available. This option is adequate for solving scalar tridiagonal systems, but for scalar pentadiagonal or block tridiagonal systems it is somewhat slower than desired. The second option is to 'transpose' the flow and geometry variables as part of the time-stepping process: Start with x-lines of data in-processor. Form explicit terms in x, then transpose so y-lines of data are in-processor. Form explicit terms in y, then transpose so z-lines are in processor. Form explicit terms in z, then solve linear systems in the z-direction. Transpose to the y-direction, then solve linear systems in the y-direction. Finally transpose to the x direction and solve linear systems in the x-direction. This strategy avoids inter-processor communication when differencing and solving linear systems, but requires a large amount of communication when doing the transposes. The transpose method is more efficient than the non-transpose strategy when dealing with scalar pentadiagonal or block tridiagonal systems. For handling geometrically complex problems the chimera strategy was adopted. For multiple zone cases we compute on each zone sequentially (using the whole parallel machine), then send the chimera interpolation data to a distributed data structure (array) laid out over the whole machine. This information transfer implies an irregular communication pattern, and is the second possible barrier to an efficient algorithm. We have implemented these ideas on the CM-5 using CMF (Connection Machine Fortran), a data parallel language which combines elements of Fortran 90 and certain extensions, and which bears a strong similarity to High Performance Fortran. We make use of the Connection Machine Scientific Software Library (CMSSL) for the linear solver and array transpose operations.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: 2nd Overset Composite Grid and Solution Technology Symposium; Oct 25, 1994 - Oct 28, 1994; Fort Walton Beach, FL; United States
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  • 84
    Publication Date: 2019-07-17
    Description: Steady and unsteady flows for propulsion systems are efficiently simulated by solving the incompressible Navier-Stokes equations. The solution method is based on the pseudo compressibility approach and uses an implicit-upwind differencing scheme together with the Gauss-Seidel line relaxation method. Current computations use one equation Baldwin-Barth turbulence model which is derived from a simplified form of the standard kappa - epsilon model equations. The resulting computer code is applied to the flow analysis inside an advanced rocket pump impeller in steadily rotating reference frames. Numerical results are compared with experimental measurements. The effects of exit and shroud cavities with the leak-age flow are investigated. Time-accurate incompressible Navier-Stokes formulation with the overlapped grid scheme capability was evaluated by using MIT flapping foil experiment. The grid dependency, turbulence model effects, and the effect of order of differencing were investigated. Numerical results were compared against experimental data. The resulting procedure were applied to unsteady flapping foil calculations. Two upstream NACA 0025 foils perform high frequency synchronized motion and generate unsteady flow conditions to the downstream larger stationary foil. Comparison between unsteady experimental data and numerical results from two different moving boundary procedures will be presented.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Workshop for CFD Applications in Rocket Propulsion; Apr 19, 1994 - Apr 21, 1994; Huntsville, AL; United States
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  • 85
    Publication Date: 2019-07-17
    Description: The diffusion controlled binary reaction between initially segregated reactants in a two-dimensional low Mach number mixing layers is studied via numerical simulation. The stoichiometric ratio of the reactants is chosen to be much larger than one, as is typical of hydrocarbon flames in air. This results is a flame that is offset from the main vortical region of the mixing layer. In agreement with experimental observations, the flame remains surprisingly uncontorted during the flow evolution and is not entrained into the mixing layer. The effect of the heat release of the flame on the evolution of the mixing layer is thus similar to the effect of a difference in free-stream density between the two sides of the layer. The resulting baroclinic torque inhibits the familiar rolup and pairing of mixing layer vortices common in constant density flows. This also contributes to the layers inability to entrain the flame. The increase in viscosity caused by the heating of the flame reduces the effective Reynolds number of the flow. But, contrary to what has commonly been suggested, this is not the major reason for the inhibition of the usual large-scale mixing layer structures.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Forty Seventh Meeting of the American Physical Society, Division of Fluid Dynamics; Nov 20, 1994 - Nov 22, 1994; Atlanta, GA; United States
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  • 86
    Publication Date: 2019-07-17
    Description: Computational fluid dynamic (CFD) analysis is performed on the Lockheed Lifting Body Single-Stage-to-Orbit vehicle to determine the heat transfer to the vehicle during its descent trajectory. Seven species, chemical nonequilibriurn computations using the GASP code will be completed at several trajectory points to assess the thermal protection requirements of the vehicle. Sophisticated surface boundary conditions including in-depth conduction, catalycity, and a variable temperature wall have been incorporated into the flow solver.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: 29th AIAA Thermophysics Conference; Jun 19, 1995 - Jun 22, 1995; San Diego, CA; United States
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  • 87
    Publication Date: 2019-07-17
    Description: MIT flapping foil experiment was used as a validation case to evaluate the current incompressible Navier-Stokes approach with overlapped grid schemes. Steady-state calculations were carried out for overlapped and patched grids. The grid dependency, turbulence model effects, and the effect of order of differencing were investigated. Numerical results were compared against experimental data. The resulting procedure were applied to unsteady flapping foil calculations. Two upstream NACA 0025 foils perform high-frequency synchronized motion and generate unsteady flow conditions to the downstream larger stationary foil. Comparison between unsteady experimental data and numerical results from two different moving boundary procedures will be presented.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: ASME Fluids Engineering Summer Meeting; Jun 19, 1994 - Jun 23, 1994; Lake Tahoe, CA; United States
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  • 88
    Publication Date: 2019-07-17
    Description: An adiabatic demagnetization refrigerator (ADR) is under development at NASA-Ames Research Center that will operate between 2 K and 10 K and will provide 50 mW of cool ng at 2 K. Gadolinium Gallium Garnet (GGG) is selected as the refrigerant for the ADR, To minimize temperature gradients in the GGG, thick slices of GGG are sandwiched together with strips of high-purity copper in between them. The copper strips are used to exchange heat between the GGG and the 2 K and the 10 K heat switches. The heat transfer across the Cu-GGG interfaces is improved by placing thin foils of' high-purity indium at the interfaces. The heat switches employed in the ADR have no moving parts. The 10 K heat switch is a helium gas-gap heat switch; while, the 2 K heat switch is a He ll-gap heat switch. A switch is on when its gap Is filled with helium and is off' when the gap is emptied. This is accomplished with an activated carbon pump (ACP). The ACP adsorbs helium when cooled and desorbs it when heated. A superconducting magnet capable of providing 9 T at 2 K is used for the ADR cycle. A prototype of this refrigerator has been built and is currently under test. A detailed design of the ADR and preliminary test results performed on the prototype ADR will be presented.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Dagstuhl Seminar on Scientific Visualization; May 22, 1994 - May 27, 1994; Saarbrucken; Germany
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  • 89
    Publication Date: 2019-07-17
    Description: Fluid dynamics of turbomachines are complicated by inherently three dimensional structures such as endwall boundary layers, hub corner separation bubbles and tip-leakage flows. In addition, the relative motion between rotors and stators causes unsteady aerodynamic interactions to occur between blade rows. It is necessary to understand the aerodynamics associated with these interactions in order to design turbomachines that are both light and compact as well as reliable and efficient. An unsteady, three-dimensional, thin-layer, Navier-Stokes zonal algorithm is used to investigate the unsteady aerodynamics of multi-stage turbines and compressors. Relative motion between rotors and stators is made possible by the use of systems of patched and overlaid grids. Time-averaged pressures and pressure envelopes have been computed for several two- and three-dimensional single- and multi-stage configurations. Flow visualizations and computed results are in good agreement with experimental data.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Department of Energy High Performance Computing and Communication Workshop on Computational Fluid Dynamics; Feb 23, 1994 - Feb 25, 1994; Seaside, OR; United States
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  • 90
    Publication Date: 2019-06-27
    Keywords: unknown
    Type: NASA-TM-X-61113 , NACA-RM-L7I05
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  • 91
    Publication Date: 2019-06-27
    Keywords: unknown
    Type: NASA-CR-92603
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  • 92
    Publication Date: 2019-07-18
    Description: Based on the geometry of Mars Environment Survey (MESUR) Pathfinder aeroshell and an estimated Mars entry trajectory, two-dimensional axisymmetric time dependent calculations have been obtained using GIANTS (Gauss-Siedel Implicit Aerothermodynamic Navier-Stokes code with Thermochemical Surface Conditions) code and CMA (Charring Material Thermal Response and Ablation) Program for heating analysis and heat shield material sizing. These two codes are interfaced using a loosely coupled technique. The flowfield and convective heat transfer coefficients are computed by the GIANTS code with a species balance condition for an ablating surface, and the time dependent in-depth conduction with surface blowing is simulated by the CMA code with a complete surface energy balance condition. In this study, SLA-561V has been selected as heat shield material. The solutions, including the minimum heat shield thicknesses over aeroshell forebody, pyrolysis gas blowing rates, surface heat fluxes and temperature distributions, flowfield, and in-depth temperature history of SLA-561V, are presented and discussed in detail.
    Keywords: Fluid Mechanics and Thermodynamics
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  • 93
    Publication Date: 2019-07-17
    Description: Up to today, preconditioning methods on massively parallel systems have faced a major difficulty. The most successful preconditioning methods in terms of accelerating the convergence of the iterative solver such as incomplete LU factorizations are notoriously difficult to implement on parallel machines for two reasons: (1) the actual computation of the preconditioner is not very floating-point intensive, but requires a large amount of unstructured communication, and (2) the application of the preconditioning matrix in the iteration phase (i.e. triangular solves) are difficult to parallelize because of the recursive nature of the computation. Here we present a new approach to preconditioning for very large, sparse, unsymmetric, linear systems, which avoids both difficulties. We explicitly compute an approximate inverse to our original matrix. This new preconditioning matrix can be applied most efficiently for iterative methods on massively parallel machines, since the preconditioning phase involves only a matrix-vector multiplication, with possibly a dense matrix. Furthermore the actual computation of the preconditioning matrix has natural parallelism. For a problem of size n, the preconditioning matrix can be computed by solving n independent small least squares problems. The algorithm and its implementation on the Connection Machine CM-5 are discussed in detail and supported by extensive timings obtained from real problem data.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: International Workshop on Solution Techniques for Large-Scale CFD Problems; Sep 26, 1994 - Sep 28, 1994; Montreal, Quebec; Canada
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  • 94
    Publication Date: 2019-07-17
    Description: A nonequilibrium, axisymmetric, Navier-Stokes flow solver with coupled radiation has been developed to use in the design of thermal protection systems for vehicles where radiation effects are important. The present method has been compared with an existing flow and radiation solver and with the Project Fire II experimental data. Very good agreement has been obtained over the entire Fire II trajectory with the experimentally determined values of the stagnation radiation intensity in the .2 to 6.2 eV range and with the total stagnation heating. The agreement was significantly better than previous numerical predictions. The effects of a number of flow models are examined to determine which combination of physical models produces the best agreement with the experimental data. These models include radiation coupling, multi-temperature thermal models, finite-rate chemistry, and a quasi-steady-state or Boltzmann assumption for the calculation of the excited electronic states. Finally, the computational efficiency of the present model is evaluated. The radiation properties model developed for this study is shown to offer significant computational savings compared to existing codes.
    Keywords: Fluid Mechanics and Thermodynamics
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  • 95
    Publication Date: 2019-07-18
    Description: Rotational temperatures have been measured in rarefied, nonequilibrium, heated freejet expansions of nitrogen using the electron beam fluorescence technique at the University of California at Berkeley Low Density Wind Tunnel facility. Spectroscopic measurements of the (0,0) band of the first negative system of nitrogen reveal the nonequilibrium behavior in the flowfield upstream of, and through the Mach disk, which forms as the freejet expands into a region of finite back pressure. Results compare well with previous freejet expansion data and computations regarding location of the Mach disk and terminal rotational temperature in the expansion. Measurements are also presented for shock thickness based on the rotational temperature changes in the flow. Thickening shock layers, departures of rotational temperature from equilibrium in the expansion region, and downstream rotational temperature recovery much below that of an isentropic normal shock provide indications of the rarefied, nonequilibrium flow behavior. The data are analyzed to infer constant values of the rotational-relaxation collision number from 2.2 to 6.5 for the various flow conditions. Collision numbers are also calculated in a consistent manner for data from other investigations for which is seen a qualitative increase with increasing temperature. Rotational-relaxation collision numbers are seen as not fully descriptive of the rarefied freejet flows. This may be due to the high degree of nonequilibrium in the flowfields, and/or to the use of a temperature-insensitive rotational-relaxation collision number model in the data analyses.
    Keywords: Fluid Mechanics and Thermodynamics
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  • 96
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    In:  Other Sources
    Publication Date: 2019-07-18
    Description: An earlier proposed constitutive relation for normal stresses originated by random particle fluctuations is used to describe a joint effect of thermal and shear-induced fluctuations on concentrational distributions in suspension flow. Averaged products of components of the fluctuation velocity are evaluated on a basis of the rational mechanics approach combined with a simple kinematic consideration. The equation of momentum conservation of the dispersed phase of a suspension closed with this constitutive relation is applied to unidirectional shear flow in the gravity field and to rotational Couette flow. Coupling of the thermal and shear-induced fluctuations results in that the ability of shear flow to suspend particles has a minimum at a certain particle size, all other things being equal. The developed model provides also for a reasonable explanation of particle distributions observed in Couette flow. The approach based on the consideration of momentum balance for the dispersed phase is proved to lead to an effective equation of convective diffusion of the suspended particles. Coefficients of mutual diffusion due to both thermal and shear-induced fluctuations are drastically different from corresponding self-diffusivities as regards both their scaling and their concentrational dependence.
    Keywords: Fluid Mechanics and Thermodynamics
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  • 97
    Publication Date: 2019-07-18
    Description: The dynamic regime of gas injection through a circular plate orifice into an ideally wetting liquid is considered, when successively detached bubbles may be regarded as separate identities. In normal gravity and at relatively low gas flow rates, a growing bubble is modeled as a spherical segment touching the orifice perimeter during the whole time of its evolution. If the flow rate exceeds a certain threshold value, another stage of the detachment process takes place in which an almost spherical gas envelope is connected with the orifice by a nearly cylindrical stem that lengthens as the bubble rises above the plate. The bubble shape resembles then that of a mushroom and the upper envelope continues to grow until the gas supply through the stem is completely cut off. Such a stage is always present under conditions of sufficiently low gravity, irrespective of the flow rate. Two major reasons make for bubble detachment: the buoyancy force and the force due to the momentum inflow into the bubble with the injected gas. The former force dominates the process at normal gravity whereas the second one plays a key role under negligible gravity conditions. It is precisely this fundamental factor that conditions the drastic influence on bubble growth and detachment that changes in gravity are able to cause. The frequency of bubble formation is proportional to and the volume of detached bubbles is independent of the gas flow rate in sufficiently low gravity, while at normal and moderately reduced gravity conditions the first variable slightly decreases and the second one almost linearly increases as the flow rate grows. Effects of other parameters, such as the orifice radius, gas and liquid densities, and surface tension are discussed.
    Keywords: Fluid Mechanics and Thermodynamics
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  • 98
    Publication Date: 2019-07-17
    Description: The occurrence of large-scale coherent structures in turbulent free shear flows (especially the planar mixing layer) has been recognized for some time. Indeed, the observation of such structures in mixing layers did much to promote interest in the study of coherent structures in turbulence. It has been widely assumed that the large-scale structures in these flows are responsible for the entrainment of free-stream fluid and the overall growth of the layer, while the small-scale structures provide mixing and dissipation. A model of scalar mixing based on these ideas was proposed for these flows. However, recent experimental and computational evidence suggests that the dominance of the large-scale structures in turbulent mixing layers is not universal. In addition, there is a substantial variation among experiments in several statistical measures of self-similar mixing layers, for example growth rate and velocity variances. To investigate the importance of large-scale structures, several free shear flows (mixing layers and wakes) have been simulated via direct numerical simulation. The simulations are designed to mimic experimental mixing layers in which the splitter plate boundary layers are turbulent. Different levels of two-dimensional forcing are included resulting in large-scale structures of differing strength and importance. These simulations are used to investigate the role of large-scale coherent structures in free shear layers and the effect of these structures on relevant turbulence statistics and scalar mixing. It is found that the statistics and structures in several experiments involving turbulent mixing layers are in better agreement with simulations that do not exhibit dominant large-scale structures than those in which the common mixing layer structures do dominate. It is also found that the level of forcing can have a profound effect on the qualitative and quantitative features of these shear layer, even when they are nominally self-similar.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: 12th U.S. National Congress of Applied Mechanics; Jun 26, 1994 - Jul 01, 1994; Seattle, WA; United States
    Format: text
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  • 99
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    In:  Other Sources
    Publication Date: 2019-07-17
    Description: Computational fluid dynamics (CFD) is beginning to play a major role in the aircraft industry of the United States because of the realization that CFD can be a new and effective design tool and thus could provide a company with a competitive advantage. It is also playing a significant role in research institutions, both governmental and academic, as a tool for researching new fluid physics, as well as supplementing and complementing experimental testing. In this presentation, some of the progress made to date in CFD at NASA Ames will be reviewed. The presentation addresses the status of CFD in terms of methods, examples of CFD solutions, and computer technology. In addition, the role CFD will play in supporting the revolutionary goals set forth by the Aeronautical Policy Review Committee established by the Office of Science and Technology Policy is noted. The need for validated CFD tools is also briefly discussed.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Computational fluid dynamics at NASA Ames Research Center; Jun 19, 1994 - Jun 20, 1994; Incline Village, NV; United States
    Format: text
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  • 100
    Publication Date: 2019-07-17
    Description: Large Dewars often use aluminum radiation shields and stainless steel vent lines. A simple, low cost method of making thermal contact between the shield and the line is to deform the shield around the line. A knowledge of the thermal conductance of such a joint is needed to thermally analyze the system. The thermal conductance of pressed metal contacts consisting of one aluminum and one stainless steel contact has been measured at 77 K, with applied forces from 8.9 N to 267 N. Both 5052 or 5083 aluminum were used as the upper contact. The lower contact was 304L stainless steel. The thermal conductance was found to be linear in temperature over the narrow temperature range of measurement. As the force was increased, the thermal conductance ranged from roughly 9 to 21 mW/K within a range of errors from 3% to 8%. Within the range of error no difference could be found between the using either of the aluminum alloys as the upper contact. Extrapolating the data to zero applied force does not result in zero thermal conductance. Possible causes of this anomalous effect are discussed.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: 15th International Cryogenic Engineering Conference and Industrial Exhibition; Jun 07, 1994 - Jun 10, 1994; Genova; Italy
    Format: text
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