摘要
根据动量守衡导出的一种快速工程计算方法,计算了超声速高超声速流中横向喷流轨迹.并对实验研究中菱形后楔面喷流进行了分析计算.给出了各种流动和几何参数的影响.
A fast engineering method is developed according to the momentum conservations. The transverse jet trajectory on supersonic and hypersonic floW is calculaed. The diamond-backface jet is analyed and calculatied,and the effects of different diameters of now and geometry are given.
基金
国家自然科学基金