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- W1980009525 abstract "¤A proof-of-concept study is performed for a supersonic channel-airfoil concept, which can be applied to the leading edges of wings, tails, � ns, struts, and other appendages of aircraft, atmospheric entry vehicles, and missiles" @default.
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- W1980009525 date "2000-03-01" @default.
- W1980009525 modified "2023-09-27" @default.
- W1980009525 title "Supersonic Channel Airfoils for Reduced Drag" @default.
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- W1980009525 doi "https://doi.org/10.2514/2.985" @default.
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