摘要
研究转速调节片对飞行转速的影响。首先计算有 /无转速调节片以及改变转速调节片特征参数等多种情况下的气动特性 ,然后仿真计算导弹的飞行转速。仿真结果表明 :转速调节片可以显著地增大导弹的导转力矩和飞行转速 ;
The influence of rotational speed adjustment board on the rotational speed in flight is studied The aerodynamic characteristic is first calculated with the rotational speed adjustment boards on or off, and in circumstances when the features of the boards are changed Then the rotational speed is simulated The simulation results show that the rotational speed adjustment boards remarkably affect the angular moment and the rotational speed in flight and that changing features of the rotational speed adjustment board can modify the extent of the effect on the rotational speed
出处
《兵工学报》
EI
CAS
CSCD
北大核心
2002年第3期355-357,共3页
Acta Armamentarii
关键词
转速调节片
飞行转速
导转力矩
导弹
尾翼安装角
rotational speed adjustment board, angular moment, rotational speed in flight
