An inlet distortion assessment during aircraft departures at high angle of attack for an F/A-18A aircraft
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Author
Contributions
- NASA Dryden Flight Research Center. - Contributor
Publication
1997 - NASA Dryden Flight Research Center, Edwards, Calif, California
Language
English
Word Count
7,250 words, Guess
Page Count
29 pages
Identifiers
- OCLC Control Number42890083
- Open LibraryOL17595886M
Subjects
Topics
Jet enginesFighter planesInlet distortionF/I 8-18A airplaneAircraft departuresHigh angle of attackEngine stability limits
Series Statement
- NASA technical memorandum -- 104328.
Links
Other Editions
- An inlet distortion assessment during aircraft departures at high angle of attack for an F/A-18A aircraft
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