二维进气道不启动流场非定常特性的混合LES/RANS模拟
Investigation on unsteady characteristics of unstarted two-dimensional inlet flow using hybrid LES/RANS method
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摘要: 采用一种混合大涡模拟/雷诺平均Navier-Stokes(LES/RANS)方程模拟方法结合5阶WENO(weighted essentially non-oscillatory)格式对马赫数为3的来流中、内收缩比为1.5的不启动状态下的二维进气道进行了计算,再现了不启动进气道中的非定常流场.计算结果表明:所采用的模拟方法对入口处的平均绝热壁温、摩擦速度和雷诺应力的计算精度较好,进气道不启动流场中激波波系和分离区存在大时空尺度的低频运动,其占主导的特征频率和典型的激波/湍流边界层干扰问题中激波和分离区的低频频率接近,且进气道出现了间歇性的启动状态.Abstract: A hybrid large-eddy simulation/Reynolds-averaged Navier-Stokes(LES/RANS) method together with 5th order WENO(weighted essentially non-oscillatory) scheme were used to caculate an unstarted two-dimensional inlet with contraction ratio of 1.5 in a Mach 3 freestream.The unsteady flow field in the unstarted inlet was captured.The result shows that current numerical method can predict mean adiabatic wall temperature,friction velocity and Reynolds stress reasonably well.Some low-frequency motion exist in the shock system and separation zone in the unstarted field at large time-space scale.The dominant frequency is close to its counterpart in classic shock/turbulent boundary layer interaction problem.The inlet switches to started state intermittently.
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