IN the March issue of AIRCRAFT ENGINEERING Mr. Falkner establishes a new power index law for the skin friction coefficient of a flat plate with fully turbulent boundary layer.
Holt, M. (1943), "Calculation of Wing Profile Drag: A New Simplified Method of Practical Value to Engineers", Aircraft Engineering and Aerospace Technology, Vol. 15 No. 10, pp. 278-280. https://doi.org/10.1108/eb031059
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