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利用迎风TVD格式,在超音速下,分别对无侧喷流和头部含侧喷流的炮弹绕流场进行数值模拟,结果表明侧喷流能够降低炮弹表面的摩擦阻力,对研究炮弹的增程技术有一定的参考价值。
Using the upwind TVD scheme, the numerical simulation of the flow field around a non-side jet and a head-side jet with supersonic velocity was carried out. The results show that the side jet can reduce the frictional resistance of the shell surface. Cheng technology has some reference value.