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Interaction between a Shock Wave and a Boundary Layer in a Nonequilibrium Hypersonic Rarefied Flow. 2nd Report. Comparison of State for Translational and Rotational Energy Distributions.

机译：极高超声波稀土流动中冲击波和边界层之间的相互作用。第二次报告。平移和旋转能量分布状态的比较。

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Nobuyuki TSUBOI; Hiroki YAMAGUCHI; Yoichiro MATSUMOTO;
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年度 2002
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1. Interaction between Shock Wave and Boundary Layer in Nonequilibrium Hypersonic Rarefied Flow (5th Report, Nonequilibrium of Rotational Temperature in Flow over Flat Plate) [J] . Nobuyuki TSUBOI, Yoichiro MATSUMOTO JSME International Journal. Series B, Fluids and Thermal Engineering . 2006,第3期

机译：非平衡高超声速稀疏流中冲击波与边界层之间的相互作用（第五次报告，平板流动的旋转温度非平衡）
2. Effects of vibrational nonequilibrium on hypersonic shock-wave/laminar boundary-layer interactions [J] . Hao Jiaao, Wen Chih-Yung International communications in heat and mass transfer . 2018,第OCTa期

机译：振动非平衡对高超声速冲击波/层状边界层相互作用的影响
3. Scaling of interaction lengths for hypersonic shock wave/turbulent boundary layer interactions [J] . Yuting HONG, Zhufei LI, Jiming YANG 中国航空学报（英文版） . 2021,第005期

机译：超声波冲击波/湍流边界层相互作用的交互长度缩放
4. Nonequilibrium Vibrational Energy Transfer Across Rarefied Hypersonic Boundary Layers [C] . G. Inger AIAA International Space Planes and Hypersonic Systems and Technologies Conference . 2008

机译：跨稀疏高超声速边界层的非平衡振动能量传递
5. Disturbances from shock/boundary-layer interactions affecting upstream hypersonic flow. [D] . Skoch, Craig Ryan. 2005

机译：来自冲击/边界层相互作用的干扰影响上游高超音速流。
6. Temporal and Spatial Evolution Characteristics of Disturbance Wave in a Hypersonic Boundary Layer due to Single-Frequency Entropy Disturbance [O] . Zhenqing Wang, Xiaojun Tang, Hongqing Lv, -1

机译：单频熵扰动引起的高超声速边界层扰动波的时空演化特征
7. Interaction between Shock Wave and Boundary Layer in Nonequilibrium Hypersonic Rarefied Flow [O] . Nobuyuki TSUBOI, Yoichiro MATSUMOTO 2006

机译：非纤维超声稀土流动冲击波和边界层之间的相互作用
8. An Analysis of Shock Structure and Nonequilibrium Laminar Boundary Layers Induced by a Normal Shock Wave in an Ionized Argon Flow. [R] . liu, w. s. 1975

机译：电离氩气流中正常冲击波引起的冲击结构和非平衡层流边界层分析。

Interaction between a Shock Wave and a Boundary Layer in a Nonequilibrium Hypersonic Rarefied Flow. 2nd Report. Comparison of State for Translational and Rotational Energy Distributions.

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