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Rocket-model investigation to determine the lift and pitching effectiveness of small pulse rockets exhausted from the fuselage over the surface of an adjacent wing at Mach numbers from 0.9 to 1.8

机译：火箭模型研究确定机身在相邻机翼表面排出的小脉冲火箭的升力和俯仰效率，马赫数为0.9至1.8

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作者
Martz, C William;
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年度 1958
页码 1-23
总页数 23
原文格式 PDF
正文语种 eng
中图分类工业技术;
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Rocket-model investigation to determine the lift and pitching effectiveness of small pulse rockets exhausted from the fuselage over the surface of an adjacent wing at Mach numbers from 0.9 to 1.8

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