Numerical study of flow and ultra narrow spectrum infrared radiation characteristics of high-altitude plume under thin atmosphere

Bao Xingdong; Yu Xilong; Wu Jie; Mao Hongxia; Wang Zhenhua; Xiao Zhihe

doi:10.3788/IRLA20200159

Volume 49 Issue S1

Sep. 2020

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Bao Xingdong, Yu Xilong, Wu Jie, Mao Hongxia, Wang Zhenhua, Xiao Zhihe. Numerical study of flow and ultra narrow spectrum infrared radiation characteristics of high-altitude plume under thin atmosphere[J]. Infrared and Laser Engineering, 2020, 49(S1): 20200159. doi: 10.3788/IRLA20200159

Citation:

Bao Xingdong, Yu Xilong, Wu Jie, Mao Hongxia, Wang Zhenhua, Xiao Zhihe. Numerical study of flow and ultra narrow spectrum infrared radiation characteristics of high-altitude plume under thin atmosphere[J]. Infrared and Laser Engineering, 2020, 49(S1): 20200159. doi: 10.3788/IRLA20200159

Numerical study of flow and ultra narrow spectrum infrared radiation characteristics of high-altitude plume under thin atmosphere

doi: 10.3788/IRLA20200159

1. State Key Laboratory of High Temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences, Beijing 100190, China;
2. School of Engineering Science, University of Chinese Academy of Sciences, Beijing 100049, China;
3. Science and Technology on Optical Radiation Laboratory, Beijing 100854, China

Received Date: 2020-03-04
Rev Recd Date: 2020-04-07
Publish Date: 2020-09-22

Abstract

The Direct Simulation Monte Carlo method was used to describe the motion, collision and energy transfer effects of a finite number of simulated molecules. The non-equilibrium flow field characteristics of the high-altitude plume were calculated, and the macroscopic parameters of the plume were obtained by statistical average method. On this basis, the Voigt line function was used to describe the broadening of the thin gas, and line-by-line integration was used to obtain the narrow-spectrum gas radiation. The physical transform equation, combined with the backward Monte Carlo method, were used to calculate the radiation transfer equations of the high-altitude plume. The applicability of the flow and radiation calculation models was verified using theoretical and experimental data. The flow and narrow spectrum infrared radiation characteristics of a small thrust engine were calculated and analyzed by using the above model. The results show that:due to the rapid expansion of the high-altitude plume, the density decreases rapidly, which leads to a significant non-equilibrium effect; the gas is affected by the velocity inertia, and the gas of different molecular weights will have a diffusion separation effect; the gas spectrum is thin and narrow, with Doppler broadening, and the peak of radiation moves to the middle wave, 4.7 μm CO and 6.5 μm H₂O emission band radiation energy account for a larger share. The radiance in the axis direction is concentrated within the distance of twice the diameter of the nozzle, while the radiance distributed in the radial direction is concentrated in the shock region and the inner flow region within the separation wave line, and the radiance in other regions decreases exponentially.
- high altitude plume,
- direct simulation Monte Carlo,
- backward Monte Carlo,
- infrared radiation

References

[1]	Simmons F S. Rocket Exhaust Plume Phenomenology[M]. California:The Aerospace Press, 2000.
[2]	Bird G A. Molecular gas dynamics and the direct simulation of gas flows[D]. New York:Oxford University Press, 1994.
[3]	Burt J M, Boyd I D. A monte carlo radiation model for simulating rarefied multiphase plume flows[R]. AIAA-2005-4691, 2005.
[4]	Kannenberg K C, Boyd I D. Three dimensional monte carlo simulation of plume impingement[R]. AIAA-1998-2755, 1998.
[5]	Gimelshein S F, Boyd I D, Ivanov M S. Modeling of internal energy transfer in plume flows of polyatomic[R]. AIAA-1999-0738, 1999.
[6]	Gatsonis N A, Nanson A R, Lebeau G J. Simulations of cold-gas nozzle and plume flows and flight data comparisons[J]. Journal of Spacecraft and Rockets, 2000, 37(1):39-48.
[7]	George J D. A combined CFD-DSMC method for numerical simulation of nozzle plume flows[D]. New York:Cornell University, 2000.
[8]	Cheng Xiaoli, Mao Mingfang, Yan Xiqin. Numerical investigations of a small thruster plume at high altitude[J]. Chinese Journal of Space Science, 2002, 22(3):261-267.(in Chinese)程晓丽, 毛铭芳, 阎喜勤. 小推力发动机高空羽流场数值模拟[J]. 空间科学学报, 2002, 22(3):261-267.
[9]	Li Zhonghua, Li Zhihui, Peng Aoping, et al. A numerical method for simulating rarefied two phase flow[J]. Acta Aerodynamic Sinica, 2015, 33(2):266-271.
[10]	Zhang Jianhua, Cai Guobiao. Computation based on the Simons model for vacuum plume[J]. Journal of Propulsion Technology, 2002, 23(5):406-409. (in Chinese)张建华, 蔡国飙. 用Simons法计算真空羽流[J]. 推进技术, 2002, 23(5):406-409.
[11]	Chen Bing, Cai Guobiao. Method of characteristics for vacuum plume simulation[J]. Journal of Propulsion Technology, 2002, 23(6):500-504. (in Chinese)陈兵, 蔡国飙. 模拟真空羽流场的特征线法[J]. 推进技术, 2002, 23(6):500-504.
[12]	Xiao Zejuan. A study of plume flow and its contamination of the space thrusters[D]. Shanghai:Shanghai Jiao Tong University, 2007. (in Chinese)肖泽娟. 空间发动机羽流及其污染研究[D]. 上海:上海交通大学, 2007.
[13]	Zheng Cailang, Zhu Dingqiang, Qiao Yaobin. Numerical simulation of the infrared radiation of orbit control thruster exhaust plume[J]. Journal of Astronautics, 2014, 35(5):521-527. (in Chinese)郑才浪, 朱定强, 乔要宾. 姿轨控发动机羽流红外辐射特性的数值仿真[J]. 宇航学报, 2014, 35(5):521-527.
[14]	Arnold J O, Whiting E E, Lyle G C. Line by line calculation of spectra from diatomic molecules and atoms assuming a voigt line profile[J]. JQSRT, 1969, 73(69):775-798.
[15]	Dong Shikui, Shuai Yong, Tan Hepin, et al. Computation of radiation heat transfer in participating media using backward Monte Carlo method[J]. Journal of Harbin Institute of Technology, 2004, 36(12):1602-1604. (in Chinese)董士奎, 帅永, 谈和平, 等. 反向蒙特卡罗法模拟参与性介质中热辐射传递[J]. 哈尔滨工业大学学报, 2004, 36(12):1602-1604.
[16]	Shuai Yong, Dong Shikui, Liu Linhua. Simulation of infrared radiation characteristics of high temperature free-stream flow including particles by using backward monte carlo method[J]. Journal of Infrared Millim Wave, 2005, 24(2):100-104. (in Chinese)帅永, 董士奎, 刘林华. 高温含粒子自由流红外辐射特性的反向蒙特卡洛方法模拟[J]. 红外与毫米波学报, 2005, 24(2):100-104.
[17]	Matthew A. Mid-infrared laser absorption diagnostics for combustion and propulsion applications[R]. N00014-07-1-0844, 2010.

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Numerical study of flow and ultra narrow spectrum infrared radiation characteristics of high-altitude plume under thin atmosphere

1. State Key Laboratory of High Temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences, Beijing 100190, China;

2. School of Engineering Science, University of Chinese Academy of Sciences, Beijing 100049, China;

3. Science and Technology on Optical Radiation Laboratory, Beijing 100854, China

Received Date: 2020-03-04

Rev Recd Date: 2020-04-07

Publish Date: 2020-09-22

Key words:

Abstract: The Direct Simulation Monte Carlo method was used to describe the motion, collision and energy transfer effects of a finite number of simulated molecules. The non-equilibrium flow field characteristics of the high-altitude plume were calculated, and the macroscopic parameters of the plume were obtained by statistical average method. On this basis, the Voigt line function was used to describe the broadening of the thin gas, and line-by-line integration was used to obtain the narrow-spectrum gas radiation. The physical transform equation, combined with the backward Monte Carlo method, were used to calculate the radiation transfer equations of the high-altitude plume. The applicability of the flow and radiation calculation models was verified using theoretical and experimental data. The flow and narrow spectrum infrared radiation characteristics of a small thrust engine were calculated and analyzed by using the above model. The results show that:due to the rapid expansion of the high-altitude plume, the density decreases rapidly, which leads to a significant non-equilibrium effect; the gas is affected by the velocity inertia, and the gas of different molecular weights will have a diffusion separation effect; the gas spectrum is thin and narrow, with Doppler broadening, and the peak of radiation moves to the middle wave, 4.7 μm CO and 6.5 μm H₂O emission band radiation energy account for a larger share. The radiance in the axis direction is concentrated within the distance of twice the diameter of the nozzle, while the radiance distributed in the radial direction is concentrated in the shock region and the inner flow region within the separation wave line, and the radiance in other regions decreases exponentially.

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Reference (17)

[1]	Simmons F S. Rocket Exhaust Plume Phenomenology[M]. California:The Aerospace Press, 2000.
[2]	Bird G A. Molecular gas dynamics and the direct simulation of gas flows[D]. New York:Oxford University Press, 1994.
[3]	Burt J M, Boyd I D. A monte carlo radiation model for simulating rarefied multiphase plume flows[R]. AIAA-2005-4691, 2005.
[4]	Kannenberg K C, Boyd I D. Three dimensional monte carlo simulation of plume impingement[R]. AIAA-1998-2755, 1998.
[5]	Gimelshein S F, Boyd I D, Ivanov M S. Modeling of internal energy transfer in plume flows of polyatomic[R]. AIAA-1999-0738, 1999.
[6]	Gatsonis N A, Nanson A R, Lebeau G J. Simulations of cold-gas nozzle and plume flows and flight data comparisons[J]. Journal of Spacecraft and Rockets, 2000, 37(1):39-48.
[7]	George J D. A combined CFD-DSMC method for numerical simulation of nozzle plume flows[D]. New York:Cornell University, 2000.
[8]	Cheng Xiaoli, Mao Mingfang, Yan Xiqin. Numerical investigations of a small thruster plume at high altitude[J]. Chinese Journal of Space Science, 2002, 22(3):261-267.(in Chinese)程晓丽, 毛铭芳, 阎喜勤. 小推力发动机高空羽流场数值模拟[J]. 空间科学学报, 2002, 22(3):261-267.
[9]	Li Zhonghua, Li Zhihui, Peng Aoping, et al. A numerical method for simulating rarefied two phase flow[J]. Acta Aerodynamic Sinica, 2015, 33(2):266-271.
[10]	Zhang Jianhua, Cai Guobiao. Computation based on the Simons model for vacuum plume[J]. Journal of Propulsion Technology, 2002, 23(5):406-409. (in Chinese)张建华, 蔡国飙. 用Simons法计算真空羽流[J]. 推进技术, 2002, 23(5):406-409.
[11]	Chen Bing, Cai Guobiao. Method of characteristics for vacuum plume simulation[J]. Journal of Propulsion Technology, 2002, 23(6):500-504. (in Chinese)陈兵, 蔡国飙. 模拟真空羽流场的特征线法[J]. 推进技术, 2002, 23(6):500-504.
[12]	Xiao Zejuan. A study of plume flow and its contamination of the space thrusters[D]. Shanghai:Shanghai Jiao Tong University, 2007. (in Chinese)肖泽娟. 空间发动机羽流及其污染研究[D]. 上海:上海交通大学, 2007.
[13]	Zheng Cailang, Zhu Dingqiang, Qiao Yaobin. Numerical simulation of the infrared radiation of orbit control thruster exhaust plume[J]. Journal of Astronautics, 2014, 35(5):521-527. (in Chinese)郑才浪, 朱定强, 乔要宾. 姿轨控发动机羽流红外辐射特性的数值仿真[J]. 宇航学报, 2014, 35(5):521-527.
[14]	Arnold J O, Whiting E E, Lyle G C. Line by line calculation of spectra from diatomic molecules and atoms assuming a voigt line profile[J]. JQSRT, 1969, 73(69):775-798.
[15]	Dong Shikui, Shuai Yong, Tan Hepin, et al. Computation of radiation heat transfer in participating media using backward Monte Carlo method[J]. Journal of Harbin Institute of Technology, 2004, 36(12):1602-1604. (in Chinese)董士奎, 帅永, 谈和平, 等. 反向蒙特卡罗法模拟参与性介质中热辐射传递[J]. 哈尔滨工业大学学报, 2004, 36(12):1602-1604.
[16]	Shuai Yong, Dong Shikui, Liu Linhua. Simulation of infrared radiation characteristics of high temperature free-stream flow including particles by using backward monte carlo method[J]. Journal of Infrared Millim Wave, 2005, 24(2):100-104. (in Chinese)帅永, 董士奎, 刘林华. 高温含粒子自由流红外辐射特性的反向蒙特卡洛方法模拟[J]. 红外与毫米波学报, 2005, 24(2):100-104.
[17]	Matthew A. Mid-infrared laser absorption diagnostics for combustion and propulsion applications[R]. N00014-07-1-0844, 2010.

Numerical study of flow and ultra narrow spectrum infrared radiation characteristics of high-altitude plume under thin atmosphere

doi: 10.3788/IRLA20200159

Abstract

References

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通讯作者: 陈斌, bchen63@163.com

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