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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.

Description

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Main Author: Hasel, Lowell E.
Language(s): English
Published: Washington D.C. : National Aeronautics and Space Administration, 1959.
Subjects: Aerodynamics, Supersonic > Aerodynamics, Supersonic / Testing.
Fighter planes > Fighter planes / Testing.
Aerodynamic load > Aerodynamic load / Testing.
Airplanes > Airplanes / Wings, Triangular > Airplanes / Wings, Triangular / Testing.
Note: "October 1959."
Cover title.
Full text also available online. Address as of 11/4/2010:
Physical Description: 116 p. : ill. ; 26 cm.
Locate a Print Version: Find in a library

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