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Kinetic comparative study on Aerodynamic Characteristics of Hypersonic Reentry Vehicle from Near-continuous Flow to Free Molecular Flow

机译：高速流入近连续流动到自由分子流动的空气动力学特性的动力学比较研究

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Jin Li; Dingwu Jiang; Xiangren Geng; Jianqiang Chen;
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年度 2021
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1. Thermal Aeroelastic Characteristics of Inflatable Reentry Vehicle Experiment (IRVE) in Hypersonic Flow [J] . Jie Wu, Zhang Zhang, Anping Hou, International journal of aerospace engineering . 2021,第a期

机译：高效流动充气再入车实验（IRVE）的热空气弹性特性
2. Backward Scattering Characteristics of a Reentry Vehicle Enveloped by a Hypersonic Flow Field [J] . Haoyu Sun, Jiajie Wang, Yiping Han, International journal of antennas and propagation . 2018,第3aSpecial期

机译：高超声速流场包围的再入飞行器的向后散射特性
3. Backward Scattering Characteristics of a Reentry Vehicle Enveloped by a Hypersonic Flow Field [J] . Sun Haoyu, Wang Jiajie, Han Yiping, International journal of antennas and propagation . 2018,第PTa2期

机译：高超声速流场包围的再入飞行器的向后散射特性
4. Free-flight aerodynamic test of reentry vehicles in high-temperature real-gas flow [C] . TANNO Hideyuki, SATO Kazuo, KOMURO Tomoyuki, AIAA international space planes and hypersonic systems and technologies conference;AIAA aviation forum . 2014

机译：再入飞行器在高温气流中的自由飞行空气动力学试验
5. Application of parabolized Navier-Stokes numerical analysis methodology in the prediction of flow field and aerodynamic properties of an air-breathing hypersonic cruise vehicle. [D] . Norman, Robert Michael. 1995

机译：抛物线型Navier-Stokes数值分析方法在空气呼吸高超音速巡航飞行器流场和空气动力学特性预测中的应用。
6. A Compact Tunable Diode Laser Absorption Spectrometer to Monitor CO2 at 2.7 μm Wavelength in Hypersonic Flows [O] . Raphäel Vallon, Jacques Soutadé, Jean-Luc Vérant, 2010

机译：紧凑型可调谐二极管激光吸收光谱仪可在高超声速流中监测2.7μm波长的CO2
7. Thermal Aeroelastic Characteristics of Inflatable Reentry Vehicle Experiment (IRVE) in Hypersonic Flow [O] . Jie Wu, Zhang Zhang, Anping Hou, 2021

机译：高效流动充气再入车实验（IRVE）的热空气弹性特性

Kinetic comparative study on Aerodynamic Characteristics of Hypersonic Reentry Vehicle from Near-continuous Flow to Free Molecular Flow

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