Large-scale low-speed wind-tunnel tests of a delta winged supersonic transport model to determine aerodynamic effects of forward or reverse thrust / by William H. Tolhurst and Kiyoshi Aoyagi.
|Main Author:||Tolhurst, William H.|
|Other Authors:||Aoyagi, Kiyoshi.|
Washington, D.C. : National Aeronautics and Space Administration, 1964.
> Wings, Triangular.
Supersonic transport planes.
Airplanes > Motors > Thrust > Testing.
Wind tunnel testing.
Full text also available online. Address as of 11/16/2010:
33 p. :
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