On the calculation of flow about objects traveling at high supersonic speeds /

A procedure for calculating three-dimensional steady and nonsteady supersonic flows with the method of characteristics is developed and discussed. An approximate method is deduced fromteh characteristics method and shown to be of practical value at high supersonic speeds

Bibliographic Details
Main Author: Eggers, A. J
Corporate Author: United States National Advisory Committee for Aeronautics
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1952
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 2811
Subjects:

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Stanford University

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Call Number: NACA TN 2811