Effect of Reynolds number on the lateral-stability derivatives at low speed of swept-back and delta-wing-fuselage combinations oscillating in yaw /
by Charles P. Llewellyn and Walter D. Wolhart.
Description
- Language(s)
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English
- Published
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Washington, D.C. : National Aeronautics and Space Administration : [1960]
- Summary
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An investigation has been made to determine the effect of Reynolds number on the lateral-stability derivatives at low speed of sweptback- and delta-wing-fuselage combinations. Results were obtained from the models oscillating in yaw over an angle-of-attack ...
- Note
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Cover title.
"August 1960."--Cover.
- Physical Description
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45 p. :
ill ;
26 cm.
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University of Illinois at Urbana-Champaign
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