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Supersonic-area-rule design and rocket-propelled flight investigation of a zero-lift straight-wing-body-nacelle configuration between Mach numbers 0.8 and 1.53

机译：超音速区域规则设计和火箭推进飞行调查的零升力直翼车身 - 机舱配置在马赫数0.8和1.53之间

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Hoffman, Sherwood;
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年度 1956
页码 1-28
总页数 28
原文格式 PDF
正文语种 eng
中图分类工业技术;
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Supersonic-area-rule design and rocket-propelled flight investigation of a zero-lift straight-wing-body-nacelle configuration between Mach numbers 0.8 and 1.53

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