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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: Fighter planes > Fighter planes / Safety measures > Fighter planes / Safety measures / Testing.
Stability of airplanes, Longitudinal > Stability of airplanes, Longitudinal / Testing.
Airplanes > Airplanes / Wings, Triangular > Airplanes / Wings, Triangular / Testing.
Delta wing airplanes > Delta wing airplanes / Stability > Delta wing airplanes / Stability / Testing.
Note: "September 1960."
Cover title.
Full text also available online. Address as of 11/15/2010:
Physical Description: 52 p. : ill. ; 26 cm.
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