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Pressure Distributions and Aerodynamic Characteristics of Several Spoiler Controls on a 40 Degree Sweptback Wing at a Mach Number of 1.61
Emma Jean LandrumK. R. Czarnecki
出版National Aeronautics and Space Administration, 1960
URLhttp://books.google.com.hk/books?id=PwcVAQAAIAAJ&hl=&source=gbs_api
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