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Rocket-powered model investigation of lift, drag, and stability of a body-tail configuration at Mach numbers from 0.8 to 2.3 and angles of attack between plus or minus 6.5 degrees

机译：火箭动力模型研究提升，阻力和体尾配置的稳定性，马赫数从0.8到2.3，攻角在正负6.5度之间

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Gillespie, Warren, Jr; Dietz, Albert E;
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年度 1954
页码 1-49
总页数 49
原文格式 PDF
正文语种 eng
中图分类工业技术 ;
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Rocket-powered model investigation of lift, drag, and stability of a body-tail configuration at Mach numbers from 0.8 to 2.3 and angles of attack between plus or minus 6.5 degrees

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