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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
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.
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- © 1956 Cambridge University Press
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