旋转子母弹后抛撒风洞试验研究
Liuti Lixue Shiyan yu Celiang/Experiments and Measurements in Fluid Mechanics（2004）
Abstract
常规兵器子母弹中,母弹旋转,子弹采用后抛撒方式抛撤.为了求得子母弹间的干扰气动力,初步发展了一套采用动力相似法准则、母弹旋转子弹抛撒的子母弹抛撒风洞模拟试验技术.结果显示,采用该技术可以求得旋转后抛撒子母弹的干扰气动力.
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Key words
Aerodynamics,Shrapnel dispersion,Wind tunnel experiment
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