Abstract
Most University students of fluid mechanics are familiar with the problem of the evaluation of the skin friction drag of a flat plate in the absence of a pressure gradient: transition is specified, usually by the free stream velocity and the transition point, or directly by the transition Reynolds number. The solution is normally obtained numerically: so far as the writer is aware, the processes used have not been written down in closed analytical form, though to do so presents no difficulty.
Publisher
Cambridge University Press (CUP)
Reference3 articles.
1. Squire H. B. and Young A. D. (1937). The Calculation of the Profile Drag of Aerofoils. R. & M. 1838, November 1937.
Cited by
6 articles.
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