A numerical simulation software is developed that can be used to simulate standing oblique detonation waves in hypervelocity flight conditions. Reasonable parameters and advanced method are provided for the application of standing detonation propulsion technology.
通过对驻定斜爆轰波形念的理论分析和数值模拟,对高超音速条件下斜爆轰波的稳定性现象进行了系统研究,探讨了产生驻定斜爆轰波的临界条件,开发了平面和锥形驻定斜爆轰波流场数值模拟软件,为驻定爆轰推进技术的应用提供合理的系统参数和先进手段。
参考来源 - 驻定斜爆轰波形态分析与数值模拟·2,447,543篇论文数据,部分数据来源于NoteExpress
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