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Aerodynamic characteristics of a group of winged reentry vehicles at Mach number 6.01 at angles of attack from 60 deg to 120 deg and minus 10 deg to 30 deg roll at 90 deg angle of attack

机译：一组有翼再入飞行器的空气动力学特性，在60度迎角下，在60度至120度和零下10度至30度的迎角下，马赫数为6.01

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作者
Goldberg, T. J.; Hondros, J. G.;
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年度 1961
页码 1-60
总页数 60
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC CHARACTERISTICS; REENTRY VEHICLES; ROLL; AERODYNAMIC COEFFICIENTS; ANGLE OF ATTACK; DRAG; TRAILING EDGES;

机译：空气动力学特征; REENTRY车辆;滚;空气动力学系数;攻击角度;拖动;拖尾边缘;

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机译：平板三角翼上的压力分布以65度的攻角从65度到115度以及从0度到25度的角度在90度迎角下以马赫数5.97扫描65度

Aerodynamic characteristics of a group of winged reentry vehicles at Mach number 6.01 at angles of attack from 60 deg to 120 deg and minus 10 deg to 30 deg roll at 90 deg angle of attack

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