Application of the method of integral relations to supersonic nonequilibrium flow past wedges and cones / by Jerry C. South, Jr.

The method of integral relations is used to calculate supersonic nonequilibrium flow past wedges and circular cones at zero incidence. Vibrational relaxation in a pure diatomic gas is considered. The governing equations are converted to approximate systems of ordinary differential equations which ar...

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Bibliographic Details
Main Author: South, Jerry C. (Jerry Curtis), 1935-
Corporate Authors: United States. National Aeronautics and Space Administration, Langley Research Center
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Aeronautics and Space Administration, 1964.
Series:NASA technical report ; R-205.
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Summary:The method of integral relations is used to calculate supersonic nonequilibrium flow past wedges and circular cones at zero incidence. Vibrational relaxation in a pure diatomic gas is considered. The governing equations are converted to approximate systems of ordinary differential equations which are solved on a high-speed digital computer as initial-value problems. Calculations are performed through the third approximation for the wedge and through the second approximation for the cone. These calculations are compared with existing calculations based on the method of characteristics.
Physical Description:31 pages : illustrations ; 27 cm.
Bibliography:Includes bibliographical references (pages 30-31)