First,hydrogen-air scramjet combustor is numerically simulated and analyzed by solving the general one-dimensional unsteady Euler equation. Second,compressible,reacting,turbulent flow solutions are obtained.

 
  • 通过求解广义一维非定常Euler方程,数值模拟了氢燃料的燃烧室,并和实验结果进行了比较和分析。
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