EFFECT OF NOSE BLUNTNESS AND CONE ANGLE ON SLENDER-VEHICLE TRANSITION - COMMENT

被引:2
|
作者
STETSON, KF
机构
[1] High Speed Aero Performance Branch, Aeromechanics Division, Flight Dynamics Laboratory, Wright Research and Development Center, OH, Wright-Patterson Air Force Base
关键词
D O I
10.2514/3.25222
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
[No abstract available]
引用
收藏
页码:1336 / 1337
页数:2
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