Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body / by William C. Sleeman, Jr., and A. Warner Robins.
|Main Author:||Sleeman, William C.|
|Other Authors:||Robins, A. Warner.|
Washington, D.C. : National Aeronautics and Space Administration, .
Angle of attack (Aerodynamics)
Stability of airplanes, Lateral.
Stability of airplanes, Longitudinal.
Airplanes > Wings, Swept-back > Testing.
Full text also available online. Address as of 11/15/2010:
62 p. :
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