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Three-dimensional Unsteady Lift Problems in High-speed Flight
Harvard LomaxMax A. HeasletFranklyn B. Fuller
其他書名
The Triangular Wing
出版National Advisory Committee for Aeronautics, 1951
URLhttp://books.google.com.hk/books?id=QZEz9QEicOkC&hl=&source=gbs_api
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註釋The indicial lift and pitching-moment coefficients are derived for flat-plate triangular wings at supersonic speeds. Coefficients are determined for angle-of-attack distributions corresponding to sinking and pitching wings. The wing with supersonic edges is completely analyzed, the wing with subsonic edges is partially analyzed; the solution in this case being completed for very narrow wings by an application of slender wing theory. In case of the supersonic edges, a comparison is made with known two-dimensional results and also with results for the same triangular wing in reversed flow.