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Compressible Flow Behind a Wing

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 June 1942

Abstract

THE changes in the relationship between the downwash behind a wing and the wing incidence in passing from flow at low values of Mach Number to flow at high values of Mach Number came to the notice of the author when investigating some high speed stressing cases.

Citation

Husk, D.I. (1942), "Compressible Flow Behind a Wing", Aircraft Engineering and Aerospace Technology, Vol. 14 No. 6, pp. 160-160. https://doi.org/10.1108/eb030911

Publisher

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MCB UP Ltd

Copyright © 1942, MCB UP Limited