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- W2021108439 abstract "The present work presents a conceptual design methodology that should indicate which high -lift device configuration satisfies a prescribed target three -dimensional maximum lift coefficient, given parametric wing sect ion information and the wing planform." @default.
- W2021108439 created "2016-06-24" @default.
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- W2021108439 date "2004-06-20" @default.
- W2021108439 modified "2023-10-05" @default.
- W2021108439 title "A Simplified Conceptual Design High-Lift Methodology for Transport Aircraft" @default.
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- W2021108439 doi "https://doi.org/10.2514/6.2004-5077" @default.
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