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- W1977604611 abstract "of the model in the wind tunnel is 5 mm. The lee surfaces were flat, whereas the leading edges were beveled at 45 deg on the windward side. The section of the wing from the apex to positions at 20%, 30%, 40%, and 50% of the chord length was hinged to deflect down relative to the rest of the wing, and the drooping angle was denoted by the symbols B1, B2, B3, and B4, respectively. This flap angle wa sv aried from 0 to 30 deg. The model is shown schematically in Fig. 1. The freestream velocity is 20 m/s, which results in a chord Reynolds number of Re = 3.16 × 10 5 ." @default.
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- W1977604611 date "2004-02-01" @default.
- W1977604611 modified "2023-09-22" @default.
- W1977604611 title "Experimental Studies on Control of Delta Wing Aerodynamics" @default.
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- W1977604611 doi "https://doi.org/10.2514/1.9101" @default.
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