Solution of the supersonic flow field around an oscillating circular cone.

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Bibliographic Details
Main Author:	Hsu, Pao-Tan
Corporate Authors:	Massachusetts Institute of Technology. Fluid Dynamics Research Laboratory, Aero-Astrodynamics Laboratory, George C. Marshall Space Flight Center, United States. National Aeronautics and Space Administration
Format:	Government Document Book
Language:	English
Published:	[Cambridge, Mass.] : M.I.T. Fluid Dynamics Research Laboratory, 1964.
Series:	NASA contractor report ; NASA CR-61064.
Subjects:	Aerodynamics, Supersonic. Noses (Aircraft)

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