Catalog Record: Effects of wing incidence on the longitudinal...

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Effects of wing incidence on the longitudinal trim characteristics of a cambered 70° delta-wing configuration at mach numbers 3.0 to 5.0 / by Warren F. Ahtye.

Main Author:	Ahtye, Warren F.
Language(s):	English
Published:	Washington, D.C. : National Aeronautics and Space Administration, 1960.
Subjects:	Delta wing airplanes > Stability > Testing. Airplanes > Wings, Triangular > Testing. Stability of airplanes, Longitudinal > Testing. Fighter planes > Safety measures > Testing.
Note:	Cover title. "September 1960." Full text also available online. Address as of 11/15/2010:
Physical Description:	52 p. : ill. ; 26 cm.
Original Format:	Book
Locate a Print Version:	Find in a library

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