CAJ | 학술논문

针对导弹箱式发射过程中燃气流对箱壁温度的影响,对导弹运动过程中燃气流场进行数值仿真,获取箱体内侧壁面附近燃气流的热物性参数,并根据燃气流场计算结果展开发射箱箱壁的传热研究.利用诺谟图法得到导弹发射过程中箱壁结构的温度变化情况,从而确定燃气流对发射箱箱体是否造成结构性的破坏,为发射箱的设计工作提供参考依据.
침대도탄상식발사과정중연기류대상벽온도적영향,대도탄운동과정중연기류장진행수치방진,획취상체내측벽면부근연기류적열물성삼수,병근거연기류장계산결과전개발사상상벽적전열연구.이용낙모도법득도도탄발사과정중상벽결구적온도변화정황,종이학정연기류대발사상상체시부조성결구성적파배,위발사상적설계공작제공삼고의거.
In order to research the effects of the jet flow on the container wall in the process of container-type missile launch, the jet flow field of the missile launch container during missile movement is simulated. Then the thermophysical parameters of jet flow near the wall are obtained. According to the numerical simulation results, the heat transfer computation is calculated and analyzed. The temperature change of the container wall in the missile launch process is obtained through the Nomogram method. The condition of temperature change will confirm whether the container is structurally damaged by the jet flow and provide valuable proposals and references to the launch container design.