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机译:一种用于超声速进气流数值模拟的新通量方案的研究
Department of Aerospace Engineering, Sharif University of Technology, Tehran, Iran;
Department of Aerospace Engineering, Sharif University of Technology, Tehran, Iran;
Engineering Research Institute, Sharif University of Technology, Tehran, Iran;
AUSM~+-up (for all speed) scheme; AUSMPW scheme; Roe scheme; supersonic intake;
机译:超声速冲流钝体上脉冲逆流射流阻力和热通量减小机理的数值研究
机译:高马赫数的3D超声速进气道中流动的数值模拟
机译:高马赫数的3D超声进气道中流动的数值模拟
机译:超音速边界层直接数值模拟的数值方案研究
机译:物质超声波和超音速流动的数值模拟
机译:基于数值平衡的格子Boltzmann方法高效的超声速流动模拟
机译:高马赫数3-D超音速摄入量流量的数值模拟
机译:超音速湍流边界层直接数值模拟数值方案研究。