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- W252587330 abstract "Abstract : A semi empirical profile-correction factor is discussed which enables the estimation of the wave drag due to thickness at supersonic speeds for three-dimensional wings with arbitrary airfoil section (subject to the restrictions of thin-airfoil theory) through use of previously calculated drag coefficients. Application of the proposed correction factor to the known drag coefficients of some rhombic-profile wings yielded estimates for the drag coefficients of parabolic-arc-profile wings that were in good agreement with theoretically calculated values. It is expected that satisfactory estimates can be obtained for many combinations of plan form and profile by judicious use of-the proposed profile correction, especially at speeds for which the wing leading edge is supersonic." @default.
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- W252587330 date "1952-02-01" @default.
- W252587330 modified "2023-09-24" @default.
- W252587330 title "Some remarks on an approximate method of estimating the wave drag due to thickness at supersonic speeds of three-dimensional wings with arbitrary profile" @default.
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