Analysis of sonic boom measurements near shock wave extremities for flight near Mach 1.0 and for airplane accelerations /
by George T. Haglund and Edward J. Kane.
|Main Author:||Haglund, George T.|
|Related Names:||Kane, Edward J.|
Washington, D.C. : National Aeronautics and Space Administration ; 1974.
Performing organization report no.: D6-22547.
iv, 128 p. :
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