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  • THERMODYNAMICS AND COMBUSTION  (344)
  • 1970-1974  (344)
  • 1971  (344)
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  • 1970-1974  (344)
Year
  • 1
    facet.materialart.
    Unknown
    In:  Other Sources
    Publication Date: 2019-08-14
    Description: Radiative heat transfer effects on small fires in zero gravity spacecraft and free falling chamber environments from diffusion flame models
    Keywords: THERMODYNAMICS AND COMBUSTION
    Type: Combustion and Flame; 16; 147-159
    Format: text
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  • 2
    Publication Date: 2019-08-14
    Description: Ablation cooling in rocket engine with combustion chamber liner and nozzle constructed of silica phenolic ablative material
    Keywords: THERMODYNAMICS AND COMBUSTION
    Type: NASA-CR-120798
    Format: application/pdf
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  • 3
    Publication Date: 2019-08-14
    Description: Measurement of smoke concentration in primary zone of gas turbine combustor at high ambient pressures by spectral radiance technique
    Keywords: THERMODYNAMICS AND COMBUSTION
    Type: NASA-TN-D-6410 , E-6083
    Format: application/pdf
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  • 4
    Publication Date: 2019-07-27
    Description: Tests were conducted on two cryogenic heat pipes using nitrogen as the working fluid. Both pipes are 1.27 cm in diameter. The first pipe is 141 cm long and uses longitudinal grooves in the aluminum wall as the wick structure. The second pipe is 91 cm long and has an arterial wick adjacent to the wall. In addition, circumferential screw threads are machined along the entire length of the inside pipe wall. Both heat pipes primed with no difficulty in the horizontal position. Start-up after burn-out was obtained repeatedly. However, more testing is required to determine whether the artery pipe is as reliable as the grooved pipe with respect to priming. Once primed, the artery heat pipe is much less sensitive to elevation than the grooved design and, consequently, offers a significant advantage with respect to ground testing. Heat-transfer characteristics of the two pipes were comparable, with both pipes achieving the initial goal of 1000 watt-cm of heat-transport capability.
    Keywords: THERMODYNAMICS AND COMBUSTION
    Type: ASME PAPER 71-WA/HT-42
    Format: text
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  • 5
    facet.materialart.
    Unknown
    In:  Other Sources
    Publication Date: 2019-07-27
    Description: A Monte Carlo modeling technique is described for mathematically simulating free molecular flows over a concave spherical surface and a concave cylindrical surface of finite length. The half-angle of the surfaces may vary from 0 to 90 degrees, and the incident flow may have an arbitrary speed ratio and an arbitrary angle of attack. Partial diffuse reflection and imperfect energy accommodation for molecules colliding with the surfaces are also considered. Results of heat transfer, drag and lift coefficients are presented for a variety of flow conditions. The present Monte Carlo results are shown to be in very good agreement with certain available theoretical solutions.
    Keywords: THERMODYNAMICS AND COMBUSTION
    Type: ASME PAPER 71-WA/HT-17
    Format: text
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  • 6
    Publication Date: 2019-07-27
    Description: Closed form, analytical solutions to the problem of steady-state heat transfer in living tissue modeled as cylindrical shells are presented and discussed. These solutions are particularly useful for the study of temperature distributions in the extremities. Metabolic heat generation, conduction, and heat transported by the blood perfusing the tissue are considered in the model. The results demonstrate the important role that the blood stream plays in the transfer of heat inside living tissue. Solutions are also presented for the limiting cases of diminishing blood flow that would occur during vasoconstriction or occlusion of blood by external means.
    Keywords: THERMODYNAMICS AND COMBUSTION
    Type: ASME PAPER 71-WA/HT-34
    Format: text
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  • 7
    facet.materialart.
    Unknown
    In:  Other Sources
    Publication Date: 2019-07-27
    Description: A heat pipe radiator consisting of 100 sodium-filled, 1.91-cm OD, stainless steel heat pipes has been tested at temperatures up to 760 C. This radiator was initially designed to have a heat pipe temperature of 740 C with a central coolant channel temperature of 771 C. The as-fabricated radiator heat pipe temperatures varied from 605 C to 700 C when the central coolant channel average temperature was 740 C. The heat pipes operated at 25 C to 110 C lower-than-expected temperatures, resulting in a 43 kW heat rejection capability vs the 50 kW design goal and the 65 kW ultimate capability of the radiator. The 43 kW heat rejection yields a mass/heat rejection ratio of 0.182 kg/kWt which is good for this early state-of-the-art heat pipe radiator. An end-of-mission life specific weight of 0.154 kg/kW is apparently achievable with improvements in radiator fabrication and brazing techniques.
    Keywords: THERMODYNAMICS AND COMBUSTION
    Type: ASME PAPER 71-WA/HT-16
    Format: text
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  • 8
    Publication Date: 2019-07-27
    Description: In order to provide a rational background for the analysis of experimental observations of blast wave phenomena, the conservation equations governing their nonsteady flow field are formulated in a general manner, without the usual restrictions imposed by an equation of state, and with proper account taken, by means of source terms, of other effects which, besides the inertial terms that conventionally dominate these equations, can affect the flow. Taking advantage of the fact that a blast wave can be generally considered as a spatially one-dimensional flow field whose nonsteady behavior can be regarded, consequently, as a function of just two independent variables, two generalized blast wave coordinates are introduced, one associated with the front of the blast wave and the other with its flow field. The conservation equations are accordingly transformed into this coordinate system, acquiring thereby a comprehensive character, in that they refer then to any frame of reference, being applicable, in particular, to problems involving either space or time profiles of the gas-dynamic parameters in the Eulerian system, or time profiles in the Lagrangian system.
    Keywords: THERMODYNAMICS AND COMBUSTION
    Type: ASME PAPER 71-WA/APM-1 , AD-739119 , AFOSR-72-0673TR
    Format: text
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  • 9
    facet.materialart.
    Unknown
    In:  Other Sources
    Publication Date: 2019-07-27
    Description: A comprehensive analysis of the Vuilleumier refrigerator was conducted. This analysis includes the effects of nonisothermal gas heat addition and rejection, hot and cold regenerator inefficiencies, conduction losses, and gas leakage losses. A computer program was written which solves the equations resulting from the analysis. The program calculates internal pressures, temperatures, and gas flow rates as functions of refrigerator crank angle, as well as overall refrigerator cooling load and power input. Comparisons between the program results and available data show good agreement, with a marked improvement over the predictions of the ideal model.
    Keywords: THERMODYNAMICS AND COMBUSTION
    Type: ASME PAPER 71-WA/HT-33
    Format: text
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  • 10
    Publication Date: 2019-07-20
    Description: Numerical analysis of effects of transient response in catalytic ignition system to promote hydrogen-oxygen combustion
    Keywords: THERMODYNAMICS AND COMBUSTION
    Type: NASA-CR-120799 , UARL-K910962-12
    Format: application/pdf
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