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.|
Washington, D.C. : National Aeronautics and Space Administration, 1960.
Delta wing airplanes
Airplanes > Wings, Triangular > Testing.
Stability of airplanes, Longitudinal > Testing.
Fighter planes > Safety measures > Testing.
Full text also available online. Address as of 11/15/2010:
52 p. :
|Locate a Print Version:||
Find in a library
- Full view (original from University of Illinois)