Low-speed investigation of the effects of frequency and amplitude of oscillation in sideslip on the lateral stability derivatives of a 60 degree delta wing, a 40 degree sweptback wing and an unswept wing /
by Jacob H. Lichtenstein and James L. Williams.
Description
- Language(s)
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English
- Published
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Washington, D.C. : National Aeronautics and Space Administration : [1961]
- Note
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Cover title.
"May 1961 ."
Aircraft; Stability and control.
- Physical Description
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19 p. :
ill. ;
26 cm.
Viewability
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University of Illinois at Urbana-Champaign
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