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Detached Eddy Simulation compared with Wind Tunnel Results of a Delta Wing with Sharp Leading Edge and Vortex Breakdown

机译:分离式涡流模拟与具有锋利的前缘和涡旋破坏的三角翼的风洞结果比较

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A delta wing configuration with a sweep angle of 65° has been investigated numerically by detached eddy simulation and compared to experimental results. In the simulations different refinement settings of the grid as well as time different time step sizes have been applied in order to reproduce the formation of the primary vortex correctly. For the comparison experimental data is available from steady and unsteady surface pressure measurements, hot wire anemometry and several other measurement techniques.
机译:通过分离涡流数值研究了掠角为65°的三角翼构型,并将其与实验结果进行了比较。在模拟中,已应用了网格的不同细化设置以及时间的不同时间步长,以便正确地再现初级涡旋的形成。为了进行比较,可以从稳态和非稳态表面压力测量,热线风速仪和其他几种测量技术中获得实验数据。

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