1) missile wing and rudder
弹翼及尾翼
1.
This paper discusses the design and the realization of missile wing and rudder electric simulation load test system based on digital signal processor(DSP) TMS320LF2407 and direct torque control(DTC) servo driver ACS600.
实验结果表明,系统能精确地模拟弹翼及尾翼在飞行展开过程中的气流阻力,满足加载测试系统的快速性要求。
2) fin-stabilized projectile
尾翼弹
1.
The analysis and Simulation of open movement about tail wing of fin-stabilized projectile Based on Matlab;
基于Matlab的尾翼弹尾翼张开的运动分析与仿真
3) bomb fin
炸弹尾翼
4) two sets of empennages bullet
双组尾翼弹
1.
Aerodynamic character calculation and analysis of two sets of empennages bullet;
双组尾翼弹气动特性计算与分析
5) fined missiles
尾翼式弹箭
6) fin-stabilized projectiles
尾翼稳定弹
补充资料：半硬壳式弹体(见弹道导弹弹体)
半硬壳式弹体(见弹道导弹弹体)
semi-hard-shelled missile body
bQn yingkeshi dan桩半硬壳式弹体(semi一hard一shelled、ssilebody)见弹道导弹弹体。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条