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Flow field survey and decelerator drag characteristics in the wake of a model of the X-15 airplane at Mach 2.30 and 4.65

机译：X-15飞机模型在2.30和4.65马赫之后的流场测量和减速器阻力特性

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Flow field survey and decelerator drag characteristics in wake of model X-15 airplane at Mach 2.30 and 4.65

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作者
Campbell, J. F.;
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年度 1966
页码 1-37
总页数 37
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AIRCRAFT MODELS; ASYMMETRY; BALLUTES; BRAKES (FOR ARRESTING MOTION); DECELERATION; DRAG; FLOW DISTRIBUTION; MACH NUMBER; SURVEYS; WAKES; WIND TUNNELS; X-15 AIRCRAFT; DECELERATION; FLOW FIELD; WIND TUNNEL; X-15 AIRCRAFT;

机译：飞机模型;不对称; BaLLUTEs;制动（争取动作）; DECELERaTION;拖动;流量分配;马赫数;调查;尾迹;风洞; X-15飞机; DECELERaTION;流场;风洞; X-15飞机;

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7. An Empirical Method for the Prediction of Airplane Drag Divergence Mach Number [O] . Roger Johnson 1953

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8. Flow Field Survey and Decelerator Drag Characteristics in the Wake of a Model of the X-15 Airplane at Mach 2.30 and 4.65 [R] . Campbell, J. F. 1966

机译：X-15飞机模型在2.30和4.65马赫的尾迹中的流场测量和减速器阻力特性

Flow field survey and decelerator drag characteristics in the wake of a model of the X-15 airplane at Mach 2.30 and 4.65

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