Effects of simulated rocket-jet exhaust on stability and control of a research-type airplane configuration at mach number of 6.86 /
by David E. Fetterman.

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Main Author
Fetterman, David E.
Related Names
United States. National Aeronautics and Space Administration.
Language(s)
English
Published
Washington, D.C. : National Aeronautics and Space Administration, [1959]
Subjects
Stability of airplanes > Testing.
Note
"October 1959."
Cover title.
Physical Description
35 p. : ill. ; 26 cm.
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Full view   University of Illinois at Urbana-Champaign