Citation: | Fu Yang’aoxiao, Liu Qingzong, Ding Mingsong, Jiang Tao, Li Peng, Dong Weizhong, Xu Yong, Gao Tiesuo. Analysis of gas model’s influence on aerodynamic characteristics for hypersonic vehicle over hot jet interaction flow field. Chinese Journal of Theoretical and Applied Mechanics, 2022, 54(5): 1229-1241. DOI: 10.6052/0459-1879-21-685 |
[1] |
董哲, 刘凯, 李旦伟等. 考虑动态控制分配的空天飞行器再入姿态复合控制设计. 宇航学报, 2021, 42(6): 749-756 (Dong Zhe, Liu Kai, Li Danwei, et al. A dynamic control al-location approach for reentry compound attitude control design of aerospace vehicle. Journal of Astronautics, 2021, 42(6): 749-756 (in Chinese) doi: 10.3873/j.issn.1000-1328.2021.06.008
|
[2] |
管再升, 阮文华, 刘伟等. 轨控推力矢量技术在防空导弹上的应用研究. 空天防御, 2020, 3(2): 1-7 (Guan Zaisheng, Ruan Wenhua, Liu Wei, et al. Study of Trajec-tory-controlled thrust vector technology application in air defense missile. Air and Space Defense, 2020, 3(2): 1-7 (in Chinese) doi: 10.3969/j.issn.2096-4641.2020.02.001
|
[3] |
Lai J, Zhao ZL, Wang XB, et al. Numerical investiga-tion of pitch motion induced unsteady effects on trans-verse jet interaction. Aerospace Science and Technology, 2020, 105: 106005 doi: 10.1016/j.ast.2020.106005
|
[4] |
张庆兵, 逯雪铃, 沙莎. 侧喷干扰高温燃气效应讨论. 实验流体力学, 2019, 33(6): 34-40 (Zhang Qingbing, Lu Xueling, Sha Sha. Effects of the high tem-perature exhaust plume reaction on lateral jet interac-tions. Journal of Experiments in Fluid Mechanics, 2019, 33(6): 34-40 (in Chinese) doi: 10.11729/syltlx20180161
|
[5] |
Zhou Z, Zhao C, Lu C, et al. Numerical studies on four-engine rocket exhaust plume impinging on flame de-flectors with afterburning. Defence Technology, 2021, 17: 1207-1216 doi: 10.1016/j.dt.2020.06.016
|
[6] |
包醒东, 余西龙, 毛宏霞等. 火箭发动机出口参数对喷焰流动及辐射的影响. 航空动力学报, 2019, 34(11): 2448-2457 (Bao Xingdong, Yu Xilong, Mao Hongxia, et al. Influence of rocket engine exit parameters on flow and radiation characteristics of exhaust plume. Journal of Aerospace Power, 2019, 34(11): 2448-2457 (in Chinese)
|
[7] |
Gnemmi P, Seiler F. Interaction of a lateral jet with the projectile external flow. AIAA Paper 2000-4196, 2000.
|
[8] |
Shingo M, Hiroki T, Kazuhisa F. Hot jet and Mach number effect on jet interaction upstream separation. AIAA Paper 2013-2977, 2013.
|
[9] |
赵弘睿, 龚安龙, 刘周等. 高空侧向喷流干扰效应数值模拟. 空气动力学学报, 2020, 38(5): 996-1003 (Zhao Hongrui, Gong Guoliang, Liu Zhou, et al. Numerical study of lateral jet interaction at high altitude. Acta Aerodynamica Sinica, 2020, 38(5): 996-1003 (in Chinese) doi: 10.7638/kqdlxxb-2020.0017
|
[10] |
Votta R, Trifonie E, Pezzella G, et al. Numerical investigation of RCS jet interaction and plume im-pingement for Mars precision landing. AIAA Paper 2017-3350, 2017.
|
[11] |
Despirito J. Effects of turbulence model on prediction of hot-gas lateral jet interaction in a supersonic crossflow. AIAA Paper 2015-1923, 2015. .
|
[12] |
林薄希, 阎超, 李亚超. 喷流干扰气动热数值模拟的若干影响因素. 北京航空航天大学学报, 2016, 42(6): 1210-1218 (Lin Boxi, Yan Chao, Li Yachao. Some influence factors in aerodynamic heat transfer numerical simulation of jet-interaction flow. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(6): 1210-1218
|
[13] |
Li Y, Reimann B, Eggers T. Coupled simulation of CFD-flight-mechanics with a two-species-gas-model for hot rocket staging. Acta Astronautica, 2016, 128: 44-61 doi: 10.1016/j.actaastro.2016.07.009
|
[14] |
Li Y, Reimann B, Eggers T. Numerical investigation on the aerodynamics of SHEFEX-III launcher. Acta As-tronautica, 2014, 97: 99-108 doi: 10.1016/j.actaastro.2014.01.006
|
[15] |
Dong H, Liu J, Chen Z, et al. Numerical investigation of lateral jet with supersonic reacting flow. Journal of Spacecraft and Rockets, 2018, 55(4): 928-935 doi: 10.2514/1.A34096
|
[16] |
赵法明. 高超声速空气化学非平衡流与燃气混合反应流场数值模拟研究. [博士论文]. 南京: 南京航空航天大学, 2019: 75-90
Zhao Faming. A numerical investigation for mixed react-ing flow-field of the air chemical nonequilibrium flow and gaseous jet flow. [PhD Thesis]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2019: 75-90(in Chinese))
|
[17] |
董维中. 热化学非平衡效应对高超声速流动影响的数值计算与分析. [博士论文]. 北京: 北京航空航天大学, 1996: 21-36
Dong Weizhong. Numerical simulation and analysis of thermal-chemical none-equilibrium effects at hypersonic flows. [PhD Thesis]. Beijing: Beijing University of Aeronautics and Astronautics, 1996: 21-36 (in Chinese)
|
[18] |
Menter FR. Two-equation eddy-viscosity turbulence models for engineering applications. AIAA Journal, 1994, 32(8): 1598-1605 doi: 10.2514/3.12149
|
[19] |
丁明松, 刘庆宗, 江涛等. 磁控热防护系统在天地往返运载器上的应用仿真. 航空学报, 2020, 42(2): 124501 (Ding Mingsong, Liu Qingzong, Jiang Tao, et al. Simulation of magnetohydrodynamic heat shield system on reusable lauch vehicle. Acta Aeronautica et Astronautica Sinica, 2020, 42(2): 124501 (in Chinese)
|
[20] |
Park C. Review of chemical-kinetic problems of future NASA missions I: earth entries. Journal of Thermophysics and Heat Transfer, 1993, 7(1): 385-398
|
[21] |
Surzhikov T, Shang JS. Kinetic models analy-sis for super-orbital aerophsics. AIAA Paper 2008-1278, 2008.
|
[22] |
Park C, Howe JT, Jaffe RL, et al. Review of chemical-kinetic problems of future NASA missions II mars entries. Journal of Thermophysics and Heat Transfer, 1994, 8(1): 9-23 doi: 10.2514/3.496
|
[23] |
Tong TW, Abou-ellail MM, Li Y. Mathematical modeling of catalytic-surface combustion of reacting flows. AIAA Paper 2006-3815, 2006.
|
[24] |
Katta VR, Roquemore WM. Simulation of dynamic jet diffusion flames using finite rate chemistry models. AIAA Journal, 1998, 36(11): 2044-2054 doi: 10.2514/2.305
|
[25] |
丛彬彬, 万田. 高速双锥绕流中热化学与输运模型影响研究. 力学学报, 2019, 51(4): 1012-1021 (Cong Binbin, Wan Tian. Effects of thermochemical and transport models on high-speed double-cone flowfield. Chinese Journal of Theoretical and Applied Mechanics, 2019, 51(4): 1012-1021 (in Chinese) doi: 10.6052/0459-1879-19-022
|
[26] |
洪启臻, 王小永, 孙泉华. 高温非平衡流动中的氧分子振动态精细分析. 力学学报, 2019, 51(6): 1761-1774 (Hong Qizhen, Wang Xiaoyong, Sun Quanhua. Detailed analysis of vibrational states of oxygen in high temperature non-equilibrium flows. Chinese Journal of Theoretical and Applied Mechanics, 2019, 51(6): 1761-1774 (in Chinese) doi: 10.6052/0459-1879-19-145
|
[27] |
丁明松, 傅杨奥骁, 高铁锁等. 高超声速磁流体力学控制霍尔效应影响. 物理学报, 2020, 69(21): 214703 (Ding Mingsong, Fu Yangaoxiao, Gao Tiesuo, et al. Influence of hall effect on hypersonic magnetohydrodynamic control. Acta Physica Sinica, 2020, 69(21): 214703 (in Chinese) doi: 10.7498/aps.69.20200630
|
[28] |
孙得川, 杨建文, 白荣博. 喷流气体性质对导弹侧向流场的影响. 空气动力学学报, 2010, 28(6): 720-723 (Sun Dewen, Yang Jianwen, Bai Rongbo. The effects of gas properties on the lateral jet interaction flowfield. Acta Aerodynamica Sinica, 2010, 28(6): 720-723 (in Chinese) doi: 10.3969/j.issn.0258-1825.2010.06.018
|
[29] |
Pao SP, Deere KA, Abdol-Hamid KS. Establishing approaches to modeling the Ares I-X and Ares I roll control system with free stream interaction. AIAA Paper 2011-1056, 2011
|
[30] |
Stahl B, Esch H, Gulhan A. Experimental inves-tigation of side jet interaction with a supersonic cross flow. Aerospace Science and Technology, 2008, 12(1): 269-275
|
[31] |
Gnemmi P, Schafer HJ. Experimental and numerical investigations of a transverse jet interaction on a missile body. AIAA Paper 2005-52, 2005
|