Investigation of the loading characteristics of the lifting surfaces and the speed brakes of a 0.067-scale model of the north american x-15 airplane (configuration 3) at Mach numbers of 2.29, 2.98, and 4.65 / by H. Norman Silvers, Julia A. Lancaster, and Jane S. Wills.
|Main Author:||Silvers, Norman H.|
|Other Authors:||Lancaster, Julia A. , Wills, Jane S.|
Washington, D.C. : National Aeronautics and Space Administration, 1960.
X-15 (Rocket aircraft)
Airplanes > Brakes > Testing.
Aerodynamic heating > Testing.
Stability of airplanes > Testing.
Wind tunnel testing.
Aeronautics > United States > Safety measures.
162 p. :
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