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  • FLUID MECHANICS AND HEAT TRANSFER  (37)
  • Inorganic Chemistry
  • 1985-1989
  • 1975-1979  (65)
  • 1950-1954
  • 1930-1934
  • 1915-1919
  • 1910-1914
  • 1976  (65)
Collection
Publisher
Years
  • 1985-1989
  • 1975-1979  (65)
  • 1950-1954
  • 1930-1934
  • 1915-1919
  • +
Year
  • 1
    Publication Date: 2016-06-07
    Description: The effect of roughness on the heat transfer distributions and the transition criteria for the windward pitch plane of the shuttle orbiter at an angle of attack of 30 deg was studied using data obtained in hypersonic wind tunnels. The heat transfer distributions and the transition locations for the roughened models were compared with the corresponding data for smooth models. The data were correlated using theoretical solutions for a nonsimilar, laminar boundary layer subject to two different flow field models for the orbiter.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: an. In Eng. Sci., Vol. 4; p 1615-1627
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  • 2
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    In:  Other Sources
    Publication Date: 2011-08-17
    Description: Drop experiments proposed for Spacelab are discussed and an acoustic chamber utilizing the torques and forces produced by acoustic waves excited within the chamber is described. Its operation and how it is being tested for experiments is discussed.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: ESA Mater. Sci. in Space; p 405-419
    Format: text
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  • 3
    Publication Date: 2019-06-27
    Description: An implicit numerical procedure was developed for predicting the transient heat flux to a material using a single embedded thermocouple. The accuracy of the method was demonstrated by comparisons with analytically generated test data.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: NASA-TM-X-58176 , JSC-10714
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  • 4
    Publication Date: 2019-06-27
    Description: An uncoupled time asymptotic alternating direction implicit method for solving the Navier-Stokes equations was tested on two laminar parallel mixing flows. A constant total temperature was assumed in order to eliminate the need to solve the full energy equation; consequently, static temperature was evaluated by using algebraic relationship. For the mixing of two supersonic streams at a Reynolds number of 1,000, convergent solutions were obtained for a time step 5 times the maximum allowable size for an explicit method. The solution diverged for a time step 10 times the explicit limit. Improved convergence was obtained when upwind differencing was used for convective terms. Larger time steps were not possible with either upwind differencing or the diagonally dominant scheme. Artificial viscosity was added to the continuity equation in order to eliminate divergence for the mixing of a subsonic stream with a supersonic stream at a Reynolds number of 1,000.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: NASA-TN-D-8217 , L-10669
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  • 5
    Publication Date: 2019-06-27
    Description: A computer program based on a finite-difference, implicit numerical integration scheme is described for the prediction of hydrogen injected into a supersonic airstream at an angle ranging from normal to parallel to the airstream main flow direction. Results of calculations for flow and thermal property distributions were compared with 'cold flow data' taken by NASA/Langley and show excellent correlation. Typical results for equilibrium combustion are presented and exhibit qualitatively plausible behavior. Computer time required for a given case is approximately one minute on a CDC 7600. A discussion of the assumption of parabolic flow in the injection region is given which demonstrates that improvement in calculation in this region could be obtained by a partially-parabolic procedure which has been developed. It is concluded that the technique described provides an efficient and reliable means for analyzing hydrogen injection into supersonic airstreams and the subsequent combustion.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: NASA-CR-2655
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  • 6
    Publication Date: 2019-07-13
    Description: An experimental study was conducted to evaluate propellant behavior in spinning toroidal tanks that could be used in a retro-propulsion system of an advanced outer-planet Pioneer orbiter. Information on propellant slosh and settling and on ullage orientation and stability was obtained. The effects of axial acceleration, spin rate, spin rate change, and spacecraft wobble, both singly and in combination, were evaluated using a 1/8-scale transparent tank in one-g and low-g environments. Liquid loadings ranged from 5% to 96% full. The impact of a surface tension acquisition device was assessed. Testing simulated the behavior of F2/N2H4 and N2O4/MMH propellants. Results are presented which indicate no major fluid behavior problems would be encountered with any of the four propellants in the toroidal tanks of a spin-stabilized orbiter spacecraft.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: AIAA PAPER 76-598 , Propulsion Conference; Jul 26, 1976 - Jul 29, 1976; Palo Alto, CA
    Format: text
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  • 7
    Publication Date: 2019-06-27
    Description: The relative ablative performance of uncoated silicone-modified reinforced carbon composite (RCC) and uncoated shuttle baseline RCC substrates was investigated. The test specimens were 13 plies (5.3 to 5.8 millimeters) thick and had a 25-millimeter-diameter test face. Prior to arc tunnel testing, all specimens were subjected to a heat treatment simulating the RCC coating process. During arc tunnel testing, the specimens were exposed to cold wall heating rates of 178 to 529 kilowatts/sq m and stagnation pressures ranging from 0.015 to 0.046 atmosphere at Mach 4.6 in air, with and without preheating in nitrogen. The results show that the ablative performance of uncoated silicone-modified RCC substrates is significantly superior to that of uncoated shuttle baseline RCC substrates over the range of heating conditions used. These results indicate that the silicone-modified RCC substrate would yield a substantially greater safety margin in the event of complete coating loss on the shuttle orbiter.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: NASA-TN-D-8358 , L-11095
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  • 8
    Electronic Resource
    Electronic Resource
    Weinheim : Wiley-Blackwell
    Berichte der deutschen chemischen Gesellschaft 109 (1976), S. 1038-1045 
    ISSN: 0009-2940
    Keywords: Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Description / Table of Contents: Synthesis of 6-Fluorobenz[a]anthracene Derivatives6-Fluoro-(12 and 6-Fluoro-12-methylbenz[a]anthracene(11) are prepared in several steps starting with 2-bromo-3-fluoronaphthalene (1). 6-Fluorobenz[a]anthracen-127H)-one (8) predominantly occurs in the enol form 9. Efforts to synthesize 6-fluoro-7,12-dimethylbenz[a]anthracene (10) are described.
    Notes: Ausgehend von 2-Brom-3-fluornapthalin (1) werden über mehrere Stufen 6-Fluor-(12) und 6-Fluor-12-methylbenz[a]anthracen (11) dargestellt. 6-Fluorbenz[a]anthracen-12(7 H)-on (8) liegt vorwiegend in der Enolform 9 vor. Syntheseversuche für 6-Fluor-7,12-dimethylbenz[a]anthracen (10) werden beschrieben.
    Type of Medium: Electronic Resource
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  • 9
    Electronic Resource
    Electronic Resource
    Weinheim : Wiley-Blackwell
    Berichte der deutschen chemischen Gesellschaft 109 (1976), S. 1465-1476 
    ISSN: 0009-2940
    Keywords: Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Description / Table of Contents: Metal Complexes of Tetrapyrrole Ligands, XVI: Methoxonitrosyl(octaethylporphinato)osmium(II)and related Osmium Complexes of OctaethylporphineThe new diamagnetic nitrosyl(octaethylporphinato)osmium (II) derivatives Os(OÄP)NO· L′(2c-e; L′ = NO, OMe, or F)2 are prepared and characterized spectroscopically. According to the electronic absorption, i.r., and 1H n.m.r. spectra fo the bis(methoxo)osmium(IV) derivative Os(OÄP)(OMe)2 (2f) and of the nitrosyls 2d, e, the latter contain OsII with an linear N≡O⊕ group and an anion OMe⊖ or F⊖ in the trans position. The strong π-acceptor NO⊕ and the strong π-donator OMe⊖ (or F⊖) effect a push-pull stabilization of the system. The dinitrosyl 2c probably shows the rare trans-array of linear M — N ≡ O⊕ and an bent M — N = O⊖ unit. The porphine ligand acts as a probe of the π-acceptor capacity of the axial ligands; in the series Py 〈 N2 〈 CO 〈 NO⊕ an increasing bathochromic shift of the α-band in the spectral region from 510 to 580 nm obtains.
    Notes: Neue, diamagnetische Nitrosyl(octaäthylporphinato)osmium(II)-Derivate OS(OÄP)NO· L′(2c bis e; L′ = NO, OMe oder F)2 werden dargestellt und spektroskopisch charakterisiert. Nach einem Vergleich der Elektronenanregungs-, IR- und 1H-NMR-Spektren des Bis(methoxo)osmium(IV) Derivats Os(OÄP)(OMe)2 (2f) und der Nitrosyl 2d, e liegt in der letzteren Os11 mit linearer N ≡ O⊕-Gruppierung und trans-ständigem Anion OMe⊖ oder F⊖ vor. Der starke π-Acceptor NO⊕ und der starke π-Donator OMe⊖ (oder F⊖) bewirken eine „push-pull“ -Stabilisierung des Systems. Im Dinitrosyl 2c light wahrscheinlich die seltene trans-Anordnung einer Linearen M—N≡O⊕- und einer gewinkelten M—N=O⊖-Einheit vor. Der Porphin-Ligand wirkt als Sonde für die π-Acceptorstärke der axialen Liganden; in der Reihe Py 〈 N2 〈 CO 〈 NO⊕ erfolgt eine zunehmend bathochrome Verschiebung der α-Bande im Spektralbereich von 510 bis 580 nm.
    Additional Material: 2 Ill.
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  • 10
    Electronic Resource
    Electronic Resource
    Weinheim : Wiley-Blackwell
    Berichte der deutschen chemischen Gesellschaft 109 (1976), S. 1163-1170 
    ISSN: 0009-2940
    Keywords: Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Description / Table of Contents: On the Evidence of Dichloroketocarbene in the Radically Induced Fragmentation of Dichlorovinylene CarbonatContrary to the thermal fragmentation of dichlorovinylene carbonate (1) the attack of sulfur radicals on 1 yields dichloromaleic acid dichloride (3), carbon dioxide, carbon oxisulfide and small amounts of dichloromaleic acid thioanhydride (6). The contested structure of 3 is confirmed by 35Cl-NQR-measurements. - Based on product formation the fragmentation very likely proceeds via dichloroketocarbene as an intermediate.
    Notes: Anders als bei rein thermischer Spaltung 2) fragmentiert Dichlorvinylencarbonat (1) beim Angriff von Schwefelradikalen zu Dichlormaleinsäuredichlorid (3), Kohlendioxid, Kohlenoxisulfid und geringen Mengen Dichlormaleinsäurethioanhydrid (6). Die bisher umstrittene Konstitution von 3 wird durch 35Cl-NQR-Messungen sichergestellt. - Der aus der Produktanalyse sich abbildende Fragmentierungsmechanismus macht das intermediäre Auftreten des Dichlorketocarbens wahrscheinlich.
    Additional Material: 1 Ill.
    Type of Medium: Electronic Resource
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