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- W2057229664 abstract "A procedure, based on the kernel function method of linearized lift ing-surf ace theory, for designing and analyzing wings in steady, low-speed flight is described. Optimized smooth surfaces were designed using this method for high lift and cruise operations. The optimization is obtained by constraining the span wise lift distribution to be elliptic. The theoretically predicted performance of the lifting surfaces was compared to wind-tunnel data. It can be inferred from the results that if high lift is the prime requirement, then it is preferable to design an optimized, smooth, high lift wing and deflect the flaps to produce a kinky cruise configuration. The application of the procedure indicates that it reduces significantly the time and expense required to generate a wing having desired characteristics." @default.
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- W2057229664 date "1970-09-01" @default.
- W2057229664 modified "2023-09-26" @default.
- W2057229664 title "Optimized design of subsonic lifting surfaces" @default.
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- W2057229664 doi "https://doi.org/10.2514/3.44197" @default.
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