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  • AIRCRAFT PROPULSION AND POWER  (2)
  • Coulomb  (1)
  • 1985-1989  (3)
  • 1985  (3)
  • 1
    Electronic Resource
    Electronic Resource
    Thermodynamics for Coulomb systems: A problem at vanishing particle densities (1985)
    Springer
    Journal of statistical physics 41 (1985), S. 975-1013 
    Details
    ISSN: 1572-9613
    Keywords: Coulomb ; thermodynamics ; quantum statistical mechanics ; partition function
    Source: Springer Online Journal Archives 1860-2000
    Topics: Physics
    Notes: Abstract In this paper I combine techniques recently developed by Charles Fefferman with the well-known methods of Joel Lebowitz and Elliott Lieb to resolve some technical problems left unsettled by Lebowitz and Lieb's fundamental 1972 paper “The constitution of matter: Existence of thermodynamics for systems composed of electrons and nuclei.”
    Type of Medium: Electronic Resource
    URL: http://dx.doi.org/10.1007/BF01010012
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    Paper (German National Licenses)
    Fulltext
  • 2
    facet.materialart.
    Unknown
    Net thrust calculation sensitivity of an afterburning turbofan engine to variations in input parameters (1985)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: The calculated value of net thrust of an aircraft powered by a General Electric F404-GE-400 afterburning turbofan engine was evaluated for its sensitivity to various input parameters. The effects of a 1.0-percent change in each input parameter on the calculated value of net thrust with two calculation methods are compared. This paper presents the results of these comparisons and also gives the estimated accuracy of the overall net thrust calculation as determined from the influence coefficients and estimated parameter measurement accuracies.
    Keywords: AIRCRAFT PROPULSION AND POWER
    Type: AIAA PAPER 85-4041
    Format: text
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    NASA TECHNICAL REPORTS
  • 3
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    Effects of inlet distortion on a static pressure probe mounted on the engine hub in an F-15 airplane (1985)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: An inlet static pressure (PS2) probe was mounted on the hub of an F100 engine in an F-15 airplane. Flight test results showed that for low distortion conditions, the ratio of engine-face total pressure to static pressure agreed well with previous altitude facility data. Off-schedule operation of the inlet third ramp angle caused increased distortion of the inlet airflow during steady-state flight conditions. Data are shown for inlet third ramp excursions leading to engine stall. The relationships of inlet face total to static pressure ratio as a function of several distortion descriptors are also described.
    Keywords: AIRCRAFT PROPULSION AND POWER
    Type: NASA-TP-2411 , H-1182 , NAS 1.60:2411
    Format: application/pdf
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    NASA TECHNICAL REPORTS
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