机译:基于腔的超音速燃烧器的大涡流/雷诺平均Navier-Stokes模拟燃烧振荡
Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha 410073, China;
Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha 410073, China;
Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha 410073, China;
Department of Mechanical Engineering, University of Sheffield, Sheffield S1 3JD, England, UK;
cavity; supersonic; combustion; oscillation;
机译:大涡/雷诺平均Navier-Stokes双模Scramjet燃烧器反应流的模拟
机译:超音速基流的雷诺平均纳维-斯托克斯/大涡模拟
机译:大涡模拟和雷诺平均Navier-Stokes模型对柴油-甲醇双燃料发动机燃烧的模拟
机译:Scramjet燃烧室流场的大涡/雷诺平均Navier-Stokes模拟
机译:定向能源应用中的混合大型涡模拟/雷诺平均Navier-Stokes建模。
机译:使用雷诺平均Navier-Stokes方程评估单个障碍物周围的气流分布和有害释放物扩散
机译:超大涡流/雷诺平均Navram-stokes模拟超燃冲压发动机燃烧室流场
机译:双模式超燃冲压发动机燃烧室的大涡/雷诺平均Navier-stokes模拟