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Analysis of Windward Side Hypersonic Boundary Layer Transition on Blunted Cones at Angle of Attack

机译:迎风角度呈浅层边界层过渡分析

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The seven-degree half-angle cone is a canonical geometry for high-speed boundary-layer transition. This paper presents constant N-Factor transition predictions for the Mack 2nd Mode along the windward plane for this geometry at differing angles of attack and differing nose radii in preparation for an upcoming experimental series. The stability analyses are able to capture the experimental trends seen in previous experiments. Computationally derived entropy swallowing lengths are shown to largely match the trends derived analytically in previous studies. These entropy swallowing lengths appear to be applicable as a figure of merit for transition studies, even at angles of attack. Bluntness appears to delay the amplification of Mack 2nd mode instabilities along the attachment line, rather than increasing the critical amplitude leading to transition. As is the case for cones at zero angle of attack, when transition occurs within the swallowing distance along the attachment line, it does not appear to be well-correlated with PSE/LST N-Factors.
机译:七度半角锥是高速边界层过渡的规范几何形状。本文呈现了沿着迎风平面的Mack第二模式的恒定的n因子转换预测,用于在不同的攻击角度和不同的鼻径半径下准备较新的实验系列。稳定性分析能够捕获先前实验中所见的实验趋势。计算衍生的熵吞咽长度显示在很大程度上与先前的研究中分析源的趋势相匹配。即使在攻击角度,这些熵吞咽长度似乎适用于过渡研究的优点。直率出现延迟麦克第二模式不稳定性的放大沿着附接线,而不是增加临界振幅导致的过渡。与零攻角处的锥体的情况一样,当沿着附接线的吞咽距离发生过渡时,它似乎与PSE / LST n因子相比良好。

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