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首页> 美国政府科技报告 >Supersonic and Transonic Wind Tunnel Tests on a Slender Ogive-Cylinder Body Single and in Combination with Cruciform Wings and Tails of Different Sizes
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Supersonic and Transonic Wind Tunnel Tests on a Slender Ogive-Cylinder Body Single and in Combination with Cruciform Wings and Tails of Different Sizes

机译：超细和跨声速风洞试验在细长的Ogive-Cylinder体单独和与不同尺寸的十字形翼和尾部结合

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Wind tunnel tests were performed at different Mach numbers on a long cylindrical body with long ogive nose. Symmetrical forces were measured for the body alone and for different combinations of body and cruciform wings of two different sizes and cruciform tails of three different sizes. For one wing and tail size two different positions of the wing were tested. Normal force and pitching moment were also measured for the two wings alone. For two model configurations some investigations were made at two Mach numbers of the effect of different boundary layer transition trips. The results were compared with results from other wind tunnels. The agreement between the results is reasonably good. (Author)

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