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On the thrust due to an air jet flowing from a wing placed in a wind tunnel

Published online by Cambridge University Press:  28 March 2006

L. C. Woods
L. C. Woods
Affiliation:
University of Sydney, Australia
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Abstract

Consider a wing-jet combination placed in a wind tunnel; the measured thrust on the wing due to a high speed jet emerging from it will require to be corrected to give the infinite stream value. This paper provides a theory of these wind tunnel corrections, and incidently establishes that the ideal thrust is almost independent of the jet exit angle.

Type
Research Article
Information
Journal of Fluid Mechanics , Volume 1 , Issue 1 , May 1956 , pp. 54 - 60
Copyright
© 1956 Cambridge University Press

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References

Allen, H. J. & Vincenti, W. G. 1944 Nat. Adv. Comm. Aero., Wash., Rep. no. 782.
Davidson, I. M. 1956 J. R. Aero. Soc. 60, 25.
Howarth, L. (ed.) 1953 Modern developments in fluid dynamics: High speed flow, vol. 2. Oxford University Press.