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Free-flight drag measurements of rocket- boosted models of two reentry body configurations at Mach numbers from 4.3 to 0.6

机译：两个再入体结构的火箭增压模型的自由飞行阻力测量，马赫数从4.3到0.6

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作者
Mc Fall, J. C., Jr.;
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年度 1959
页码 1-25
总页数 25
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC DRAG; DRAG MEASUREMENT; FLIGHT TESTS; REENTRY VEHICLES; SCALE MODELS; AERODYNAMIC CHARACTERISTICS; AERODYNAMIC CONFIGURATIONS; LIFT DRAG RATIO;

机译：空气动力学; DRaG测量;飞行测试; REENTRY车辆;尺度模型;空气动力学特征;空气动力学配置;升降比;

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Free-flight drag measurements of rocket- boosted models of two reentry body configurations at Mach numbers from 4.3 to 0.6

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