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The author here studied the effects of both leading edge bluntness and Reynolds number to aerodynamic characteristics of delta wings, through numerical simulation. 本文通過(guò)數(shù)值模擬的方法，研究了三角翼前緣鈍度和雷諾數(shù)對(duì)三角翼氣動(dòng)特性的影響。