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 . the main points are as follows : the mathematical model is developed that can be used to analyze the properties of planar standing oblique detonation waves 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。
