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Abstracts from the Scientific and Technical Press, No. 99, February, 1942

Published online by Cambridge University Press:  28 July 2016

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Abstract

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Abstract
Copyright
Copyright © Royal Aeronautical Society 1942

References

Note on page 104 * Reorit=U∞ δ/γ where δ = displacement thickness of boundary layer. If Re<Reorit for a given velocity profile, small disturbances of any frequency are ultimately damped out.

Note on page 111 * R.T.P. translation No. 1414. (Abstract supplied by Research Dept. Met. Vick.)