An edition of Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft (1999)

Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft
Factors affecting inlet-engine compatibility ...
W.G. Steenken ... [et al.].
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Last edited by MARC Bot
February 7, 2019 | History
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An edition of Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft (1999)

Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft

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Publish Date
Publisher
National Aeronautics and Space Administration, Dryden Flight Research Center, National Technical Information Service, distributor
Language
English

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Subjects

F-18 aircraft, Compressors, Subsonic speed, Aerodynamic stability, Angle of attack, Flight control, Research vehicles, Rotors, Control surfaces

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Edition Availability
Cover of: Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft
Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft
1999, National Aeronautics and Space Administration, Dryden Flight Research Center, National Technical Information Service, distributor
Microform in English
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Book Details

Edition Notes

Shipping list no.: 99-0685-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1999] 3 microfiches.

Published in
Edwards, Calif, Springfield, VA
Series
NASA/TM -- 1999-206572., NASA technical memorandum -- 206572.
Other Titles
Factors affecting inlet engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft.

The Physical Object

Format
Microform
Pagination
1 v.

ID Numbers

Open Library
OL17839405M
OCLC/WorldCat
41964667

Source records

Oregon Libraries MARC record

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February 7, 2019 Created by MARC Bot import existing book