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
Published
1996
by National Aeronautics and Space Administration, Langley Research Center, National Technical Information Service, distributor in Hampton, Va, [Springfield, Va
.
Written in English
Edition Notes
| Other titles | High speed engine component performance assessment using exergy and thrust-based methods. |
| Statement | D.W. Riggins. |
| Series | NASA contractor report -- 198271., NASA contractor report -- NASA CR-198271. |
| Contributions | Langley Research Center. |
| The Physical Object | |
|---|---|
| Format | Microform |
| Pagination | 1 v. |
| ID Numbers | |
| Open Library | OL18086871M |
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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]
