missile aerodynamics造句

• Lateral jet control technology is researched in this dissertation , based on supersonic / hypersonic missile aerodynamics and lateral jet interaction ( ji ) effects associated with the attitude control solid - propellant rocket motors system in the low endoatmospheric range
  横向喷流干扰效应研究在超声速高超声速导弹总体设计和精确制导技术研究领域一直占有重要地位。本论文针对大气层内超声速高超声速导弹采用姿态固体火箭发动机侧喷流控制技术的一些问题进行了研究。