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。
参考来源 - 大气层内拦截弹侧向喷流控制技术研究·2,447,543篇论文数据，部分数据来源于NoteExpress
给出了计算横向喷流气动干扰力的数学方法。
Furthermore, a mathematical method calculating the aerodynamic disturbing force of transverse jet stream is presented.
本文探讨了超声速平板横向喷流干扰湍流流场的数值模拟方法。
A numerical method of the supersonic turbulent flow on the flat plate interacted by supersonic lateral jet is presented in this paper.
由于喷流方向与主流方向夹角较小，总压损失也较物理斜坡、横向喷流等混合增强方式小。
Due to the smaller Angle of injection, the ratio of total pressure loss of aerodynamic ramp is less than the physical ramp and transverse injection stream.
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