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 /

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Bibliographic Details
Author / Creator:Steenken, William G., author.
Imprint:Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, February 1999.
Description:1 online resource (vii, 191 pages) : illustrations.
Language:English
Series:NASA/TM ; 1999-206572
NASA technical memorandum ; 1999-206572.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/11545454
Hidden Bibliographic Details
Other authors / contributors:Dryden Flight Research Facility, issuing body.
Notes:"February 1999."
"Performing organization: NASA Dryden Flight Research Center"--Report documentation page.
Includes bibliographical references (page 34).
Technical memorandum.
Prepared for NASA Dryden Flight Research Center WU 529-31-04-00-37-00-F18 H-2327
Description based on online resource; title from PDF title page (NASA, viewed Aug. 18, 2017).
Other form:Microfiche version: Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft
GPO item no.:0830-D (online)
Govt.docs classification:NAS 1.15:206572
Description
Item Description:"February 1999."
"Performing organization: NASA Dryden Flight Research Center"--Report documentation page.
Physical Description:1 online resource (vii, 191 pages) : illustrations.
Bibliography:Includes bibliographical references (page 34).

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