NASA NACA-TN-3671-1956 Wind-tunnel investigation of the effect of clipping the tips of triangular wings of different thickness camber and aspect ratio - transonic bump method《使用跨音速.pdf

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NASA NACA-TN-3671-1956 Wind-tunnel investigation of the effect of clipping the tips of triangular wings of different thickness camber and aspect ratio - transonic bump method《使用跨音速.pdf

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