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F. Roos

Bio: F. Roos is an academic researcher. The author has contributed to research in topics: Shock wave. The author has an hindex of 1, co-authored 1 publications receiving 1 citations.
Topics: Shock wave

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Proceedings ArticleDOI


15 Jan 1979

1 citations

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01 Jan 1982
TL;DR: In this paper, the authors defined the normal force and pitch moment coefficients of a wing span and its chord, and the slope of a section normal force vs angle-of-a attack curve.
Abstract: Nomenclature b = wing span c = wing chord c , = section drag coefficient d c = section lift coefficient c = section normal force coefficient n c = slope of section normal force vs angle-ofa attack curve c = section pitching moment coefficient C = aircraft drag coefficient C = aircraft lift coefficient LI C = pressure coefficient Cju = blowing coefficient M = Mach number P = total pressure q , q = freestream dynamic pressure

5 citations