Impact of dissociation and sensible heat release on pulse detonation and gas turbine engine performance
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Author
Contributions
- NASA Glenn Research Center. - Contributor
Publication
2001 - National Aeronautics and Space Administration, Glenn Research Center, Cleveland, Ohio, Ohio
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Identifiers
- OCLC Control Number50794141
- Open LibraryOL17607448M
Subjects
Topics
Series Statement
- [NASA technical memorandum] -- NASA/TM-2001-211080.
- NASA technical memorandum -- 211080.
Links
Other Editions
- Impact of dissociation and sensible heat release on pulse detonation and gas turbine engine performance
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