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- W24969053 abstract "In the course of a larger survey of some aerodynamic characteristics of a family of sweptback wings, the low-speed lift distributions were calculated. The 35 planforms considered cover a range of leading-edge sweep angles from 55° to 70°, and aspect ratios from 2 to 3.9. The results are given here, together with a comparison with other calculations and with experimental results on one particular wing." @default.
- W24969053 created "2016-06-24" @default.
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- W24969053 date "1962-08-31" @default.
- W24969053 modified "2023-09-27" @default.
- W24969053 title "Calculated lift distributions in compressible flow on some sweptback wings" @default.
- W24969053 hasPublicationYear "1962" @default.
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