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A free-flight investigation of the effects of a sonic jet on the total-drag and base-pressure coefficients of a boattail body of revolution from Mach number 0.83 to 1.70

机译：自由飞行研究声波射流对马赫数为0.83到1.70的船尾旋转体的总阻力和基础压力系数的影响

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Falanga, Ralph A;
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年度 1956
页码 1-18
总页数 18
原文格式 PDF
正文语种 eng
中图分类工业技术;
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A free-flight investigation of the effects of a sonic jet on the total-drag and base-pressure coefficients of a boattail body of revolution from Mach number 0.83 to 1.70

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