In this thesis, the aerodynamic heating methods of hypersonic projectile are presented.
本论文进行了高超声速弹丸的气动热研究.
网络文摘精选
Flying aerodynamic heating makes great effect on the reliability of nose fuze.
飞行气动热对弹头引信可靠性影响极大.
互联网摘选
采用工程估算方法, 计算了近程高速弹头的非定常气动加热.
互联网摘选
这类弹丸在大气中高速飞行,并受到剧烈的气动加热及空气动力负荷的作用.
互联网摘选
