An edition of Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept (1989)

Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept

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Low-speed wind-tunnel study of reaction contr ...
Donald R. Riley, Donald R. Ril ...
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Last edited by WorkBot
January 19, 2010 | History
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An edition of Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept (1989)

Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept

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Publish Date
Publisher
National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, For sale by the National Technical Information Service]
Language
English
Pages
36

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Subjects

Control systems, Testing, Airplanes, Short take-off and landing aircraft, Hovering, Vertically rising aircraft, Vertical takeoff aircraft, Reaction jets, Jet flow, Wind tunnel tests, Short takeoff aircraft, Fighter aircraft, Attitude control
Edition Availability
Cover of: Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept
Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept
1989, National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, For sale by the National Technical Information Service]
in English
Cover of: Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept
Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept
1989, Langley Research Center
Cover of: Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept
Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept
1989, National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, For sale by the National Technical Information Service]
Microform in English
Cover of: Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept
Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept
1989, National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, For sale by the National Technical Information Service]
Microform in English

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Book Details

Edition Notes

Shipping list no.: 90-0669-M.

"Performing organization report no.: L-16616"--Technical rept. documentation p.

Includes bibliographical references (p. 11).

Also available via Internet from the NASA Technical Report Server web site. Address as of 7/28/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900002435%5F1990002435.pdf; current access available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1990] 1 microfiche : negative.

505-61-71-07.

Published in
[Washington, D.C.], [Springfield, Va
Series
NASA technical memorandum -- 4147.
Other Titles
Low speed wind tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept.

The Physical Object

Pagination
36 p. :
Number of pages
36

Edition Identifiers

Open Library
OL17630289M
OCLC/WorldCat
24899982

Work Identifiers

Work ID
OL11147790W

Source records

Oregon Libraries MARC record

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History

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January 19, 2010 Edited by WorkBot add subjects and covers
December 11, 2009 Created by WorkBot add works page