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Transonic wind-tunnel investigation of the effect of control span and large wing-tip nacelles on effectiveness of spoiler-slot-deflector controls on an unswept-wing fighter-type airplane /
by Dewey E. Wornom.



Main Author: Wornom, Dewey E.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration, 1960.
Subjects: Transonic wind tunnels > Transonic wind tunnels / Testing.
Spoilers (Airplanes) > Spoilers (Airplanes) / Handling characteristics > Spoilers (Airplanes) / Handling characteristics / Testing.
Airplanes > Airplanes / Nacelles > Airplanes / Nacelles / Handling characteristics > Airplanes / Nacelles / Handling characteristics / Testing.
Fighter planes > Fighter planes / Performance > Fighter planes / Performance / Testing.
Research aircraft > Research aircraft / Design and construction > Research aircraft / Design and construction / Testing.
Note: "Langley Research Center, Langley Field, Va."
"NASA TM X-280."
Cover title.
Also available online as a PDF file via the NASA Technical Reports Server (NTRS) website. Address as of 11/2/2010:
Physical Description: 29 p. : ill. ; 26 cm.
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