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  • Other Sources  (3)
  • MATHEMATICS AND INFORMATION SCIENCES  (2)
  • AERODYNAMICS  (1)
  • 1980-1984  (1)
  • 1965-1969  (2)
  • 1
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    Propellant tank pressurization analysis program (1967)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: Computer program for the analysis of a single propellant tank pressurization system includes many pertinent physical phenomena previously ignored in other mathematical models. This program can be used for analysis, simulation, and design of propellant pressurization systems.
    Keywords: MATHEMATICS AND INFORMATION SCIENCES
    Type: MFS-1506
    Format: application/pdf
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
  • 2
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    Propellant tank pressurization analysis program (1969)
    In:  Other Sources
    Details
    Publication Date: 2019-06-27
    Description: Propellant tank pressurization analysis program considers fluid densities related to pressures and temperatures acting on the components, heat transfer between the fluids, the components, the ambient, plus component volumes, materials, and configurations in the formation of a mathematical model. This program is written in FORTRAN H and MAP.
    Keywords: MATHEMATICS AND INFORMATION SCIENCES
    Type: MFS-12623
    Format: text
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
  • 3
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    Time resolved measurements in a low aspect ratio transonic compressor stage (1982)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: The time resolved flowfield in a low aspect ratio transonic compressor stage has been studied using a high frequency response sphere probe with a bandpass of D.C. to 20 kHz in a blowdown compressor facility. Averaged over the compressor annulus, the data agree well with those measured with standard pitot type probes on the same stage in a conventional test rig. Not all the spanwise distributions agree, however. These differences are explained as errors in the pitot probe readings due to fluctuations in the flow. The experimental data are compared to the results of a three-dimensional inviscid Euler calculation.
    Keywords: AERODYNAMICS
    Type: ASME PAPER 82-GT-201 , International Gas Turbine Conference and Exhibit; Apr 18, 1982 - Apr 22, 1982; London
    Format: text
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    NASA TECHNICAL REPORTS
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