An inlet distortion assessment during aircraft departures at high angle of attack for an F/A-18A aircraft
By: William G. Steenken ... [et al.].
Contributors: NASA Dryden Flight Research Center.
Series: NASA technical memorandum -- 104328.
Publisher: NASA Dryden Flight Research Center; National Technical Information Service, distributor]
Published: 1997
Place of publication: Edwards, Calif; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 29
Subjects: Jet engines.; Fighter planes.; Aircraft departures.; Engine stability limits.; F/I 8-18A airplane.; High angle of attack.; Inlet distortion.
Notes: Shipping list no.: 1997-0768-M.

"NASA High-Angle-of-Attack Technology Conference, NASA Langley Research Center, Hampton, Virginia, September 17-19, 1996."

Includes bibliographical references (p. 7-8).

Also available via Internet from the NASA Web site. Address as of 9/09/04: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19970012654%5F1997021272.pdf; current access available via PURL.

Microfiche. [Washington, D.C.] : Supt. of Docs., U.S. G.P.O., [1997] 1 microfiche : negative.