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Wind-tunnel investigation at high subsonic speeds to determine stability and control characteristics of antitank missiles with ram-pressure jet controls on a ring tail

机译：高亚音速下的风洞调查确定反坦克导弹的稳定性和控制特性，环形尾部采用冲压喷射控制

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High subsonic wind tunnel study of stability and control characteristics of antitank missile with ram-pressure jet controls on ring tail

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作者
Vogler, R. D.;
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年度 1960
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
ANTITANK MISSILES; JET CONTROL; STABILITY; SUBSONIC SPEED; SUBSONIC WIND TUNNELS; TAIL ASSEMBLIES; WIND TUNNELS; ANTITANK MISSILE; JET CONTROL; STABILITY AND CONTROL; TAIL ASSEMBLY; WIND TUNNEL;

机译：aNTITaNK mIssILEs;喷射控制;稳定性; sUBsONIC spEED; sUBsONIC WIND TUNNELs; TaIL assEmBLIEs;风洞; aNTITaNK mIssILE;喷射控制;稳定性和控制; TaIL assEmBLY;风洞;

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7. Numerical and Experimental Determination of Canard Controlled Missile Aerodynamic Coefficients in Subsonic Regime [O] . 2019

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Wind-tunnel investigation at high subsonic speeds to determine stability and control characteristics of antitank missiles with ram-pressure jet controls on a ring tail

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