An experimental pressure-distribution investigation of interference effects produced at a Mach number of 3.11 by wedge- shaped bodies located under a triangular wing /
by Lowell E. Hasel.
|Main Author:||Hasel, Lowell E.|
Washington D.C. : National Aeronautics and Space Administration, 1959.
Aerodynamics, Supersonic /
Fighter planes > Fighter planes / Testing.
Aerodynamic load > Aerodynamic load / Testing.
Airplanes > Airplanes / Wings, Triangular > Airplanes / Wings, Triangular / Testing.
Full text also available online. Address as of 11/4/2010:
116 p. :
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|Full view||University of Illinois at Urbana-Champaign|