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- W2030429762 abstract "A linearized panel method program developed for the design and analysis of wing-body configurations at supersonic speeds (Woodward 1) has been modified to permit the user to specify the loading for an arbitrary region of the wing. The remaining portion of the wing is then optimized on the basis of the prescribed loading. This insures that the final shape will produce the minimum drag possible within the constraints. In addition, the design feature has been incorporated into an improved panel method supersonic analysis program (Woodward II). Since this code has the capability of representing bodies of noncircular cross section, it is expected to prove useful in the design of aircraft configurations with arbitrarily shaped fuselages. Comparisons are presented with other known minimum drag solutions which demonstrate the validity of both new techniques." @default.
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- W2030429762 date "1980-02-01" @default.
- W2030429762 modified "2023-09-25" @default.
- W2030429762 title "Advances in Supersonic Configuration Design Methods" @default.
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- W2030429762 doi "https://doi.org/10.2514/3.57882" @default.
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