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Supersonic flow over an inclined wing of zero aspect ratio

Published online by Cambridge University Press:  24 October 2008

K. Stewartson
K. Stewartson
Affiliation:
St Catharine's CollegeCambridge
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Abstract

An asymptotic expression is found for the lift distribution on a long, narrow, laminar wing, at incidence in a supersonic stream. The approximations of the linearized potential theory are used.

Type
Research Article
Information
Mathematical Proceedings of the Cambridge Philosophical Society , Volume 46 , Issue 2 , April 1950 , pp. 307 - 315
Copyright
Copyright © Cambridge Philosophical Society 1950

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References

REFERENCES

(1)Gunn, J. C.Philos. Trans. 240 A (1948), 327.Google Scholar
(2)Schwabzschild, K.Math. Ann. 55 (1902), 177.CrossRefGoogle Scholar
(3)Ward, G. N.Quart. J. Mech. Appl. Math. 1 (1948).CrossRefGoogle Scholar