首页> 外文会议>Proceedings of the 7th European symposium on aerothermodynamics. >LARGE EDDY SIMULATIONS OF THE 3D SUBSONIC INCOMPRESSIBLE ANDTURBULENT FLOW OVER A FIXED RE-ENTRY CAPSULE AT RE = 10 000
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LARGE EDDY SIMULATIONS OF THE 3D SUBSONIC INCOMPRESSIBLE ANDTURBULENT FLOW OVER A FIXED RE-ENTRY CAPSULE AT RE = 10 000

机译:在RE = 10000的固定重入胶囊上的3D亚音速不​​可压缩和湍流的大涡模拟

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Large eddy simulations (LES) of the 3D turbulent flowrnover a fixed re-entry capsule at Re = 104 and at a 180u000ernangle of attack have been performed with the axisymmetricrnversion of a combined spectral/stabilized finite elementrnincompressible flow solver called SFELES. Thesernsimulations allow the visualization of a large recirculatingrnzone in the wake of the capsule, which is characterizedrnby a meandering ‘fish tail' flapping motion. The detachmentrnof the boundary layer at the sphere-cone junctionrnof the capsule appears also clearly, resulting in arnstrong shear layer and a fully separated flow surface inrnthe aft conical part of the capsule. Due to the developmentrnof Kelvin-Helmholtz instabilities, this shear layerrnrolls up and give rise to a vortex ring shedding. The mainrnfrequencies of these phenomena are captured by meansrnof power spectrum densities (PSD) associated with therntemporal evolution of local physical variables. The aerodynamicrncoefficients are also computed and their PSDrnreveal that the static stability of the capsule is characterizedrnby low frequencies related to the ‘fish tail' flappingrnmotion of the wake and to some instabilities in the shearrnlayer.
机译:使用组合的频谱/稳定有限元不可压缩流求解器的轴对称变换对3D湍流绕过Re = 104固定回折胶囊并以180u000攻角进行大涡模拟(LES)。通过这些模拟,可以看到胶囊尾部有较大的再循环区域,其特征是蜿蜒的“鱼尾”拍打动作。胶囊在球体与圆锥体交界处的边界层的分离也清晰可见,从而在胶囊的锥形部分后方产生了阿恩斯特朗剪切层和完全分离的流动表面。由于Kelvin-Helmholtz不稳定性的发展,该剪切层卷起并引起涡旋环脱落。这些现象的主要频率是通过与局部物理变量的时间演变相关的平均功率谱密度(PSD)来捕获的。还计算了空气动力学系数,并通过PSD揭示了舱室的静态稳定性,其特征在于低频与尾流的“鱼尾”拍打运动以及剪切层中的某些不稳定性有关。

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