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Analytical solutions for Prandtl-Meyer wave-oblique shock overtaking interaction

Article ID Journal Published Year Pages File Type
8056949 Acta Astronautica 2014 9 Pages PDF
Abstract
The results obtained can be used for the design of re-entry capsules, supersonic inlets, and supersonic nozzles, where wave interactions considered in the present paper take place.
Keywords
Supersonic flowAnalytical solutions
Related Topics
Physical Sciences and Engineering Engineering Aerospace Engineering
Preview
Analytical solutions for Prandtl-Meyer wave-oblique shock overtaking interaction
Authors
M.V. Silnikov, M.V. Chernyshov, V.N. Uskov,
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Journal: Acta Astronautica
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