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Tuesday, August 11, 2020 | History

3 edition of High-speed engine/component performance assessment using exergy and thrust-based methods found in the catalog.

High-speed engine/component performance assessment using exergy and thrust-based methods

High-speed engine/component performance assessment using exergy and thrust-based methods

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  • 20 Currently reading

Published by National Aeronautics and Space Administration, Langley Research Center, National Technical Information Service, distributor in Hampton, Va, [Springfield, Va .
Written in English

    Subjects:
  • Brayton cycle.,
  • Engine parts.,
  • Engine tests.,
  • Performance tests.,
  • Supersonic combustion ramjet engines.,
  • Thrust.

  • Edition Notes

    Other titlesHigh speed engine component performance assessment using exergy and thrust-based methods.
    StatementD.W. Riggins.
    SeriesNASA contractor report -- 198271., NASA contractor report -- NASA CR-198271.
    ContributionsLangley Research Center.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL18086871M


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High-speed engine/component performance assessment using exergy and thrust-based methods Download PDF EPUB FB2

Get this from a library. High-speed engine/component performance assessment using exergy and thrust-based methods. [D W Riggins; Langley Research Center.]. The energy and exergy methods in practice: High-speed engine/component performance assessment using exergy and thrust-based.

methods, NASA-CR High-Speed Engine/Component Performance Assessment Using Exergy and Thrust-Based Methods. This is an ex-library book and may have the usual library/used-book markings book has hardback covers.

In good all round condition. Dust Jacket in good condition. Please note the Image in this listing is a stock photo and may not match the. Riggins, D. W., “Brayton Cycle Engine/Component Performance Assessment Using Exergy and Thrust-Based Methods”, AIAA PaperJuly Riggins, D. W., "The Evaluation of Performance Losses in Multi-Dimensional Propulsive Flows," AIAA PaperJanuary A comparative study of high-speed engine performance assessment techniques based on exergy (available work) and thrust potential (thrust availability) is summarized.

Riggins DW () High-speed engine/component performance assessment using exergy and thrust-based methods, NASA-CR, January Google Scholar Roth BA, Mavris DN () A comparison of thermodynamic loss Cited by: 1. High-speed engine/component performance assessment using exergy and thrust-based methods, NASA-CR, January.

Roth, B.A., Mavris, D.N. A comparison of thermodynamic loss models applied to the J79 Turbojet Engine; Joint Propulsion Conference and Exhibit, 36th, Huntsville, July, AL, pp– SomeExergeticMeasuresofaJT8DTurbofanEngineOnderTuranFacultyofAeronauticsandAstronauticsAnadoluUniversityTREskisehirTurkeyEmail:[email protected]