The comparison indicates that the source term method can predict pressure distribution of the combustor and can meet the need of the vehicle configuration and integral design.

• 与直联式试车台实验数据对比表明，该方法能够较好地模拟冲压发动机内压力分布，能够满足飞行器气动／推进一体化构型方案设计及总体方案设计阶段的需求。