首页> 外文会议>AIAA 33rd Aerospace Seicnces Meeting and Exhibit January 9-12, 1995/Reno, NV >Numerical investigation of laminar-turbulent transition in the boundary-layer of reentry capsules
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Numerical investigation of laminar-turbulent transition in the boundary-layer of reentry capsules

机译:再入舱边界层内层流湍流过渡的数值研究

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摘要

Transition from laminar to turbulent flow in the boundary layer of blunt bodies under reentry conditions from space is investigated using the tool of numerical simulation. In particular the relevant flow instability mechanisms are investigated with the aim to develop new instability based transition criteria.
机译:利用数值模拟工具,研究了从空间再入条件下钝体边界层中层流向湍流的过渡。尤其是,研究了相关的流量不稳定机制,目的是开发新的基于不稳定的过渡标准。

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