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Correction to Smyrl's results for thin yawed wedges

Published online by Cambridge University Press:  29 March 2006

N. L. Arora
Affiliation:
Department of Aeronautical Engineering, Delft University of Technology, Delft Present address: Indian Institute of Technology, Kanpur.

Abstract

It is the purpose of this note to correct Smyrl's (1963) results for the perturbation pressure in the interaction field produced behind a plane shock which is being diffracted by a supersonically moving thin yawed wedge.

Type
Research Article
Copyright
© 1970 Cambridge University Press

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References

Arora, N. L. 1968 J. Fluid Mech. 34, 209.
Arora, N. L. 1969 Tech. Univ. Delft Report VTH-158.
Smyrl, J. L. 1963 J. Fluid Mech. 15, 223.