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美国政府科技报告
>Effects of spoiler on airfoil pressure distribution and effects of size and location of spoilers on the aerodynamic characteristics of a tapered unswept wing of aspect ratio 2.5 at a Mach number of 1.90
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Effects of spoiler on airfoil pressure distribution and effects of size and location of spoilers on the aerodynamic characteristics of a tapered unswept wing of aspect ratio 2.5 at a Mach number of 1.90