Establishment of narrow spectral band model parameters database for gas high temperature radiation characteristics

Cai Honghua; Nie Wansheng; Wu Rui; Su Lingyu; Hou Zhiyong

doi:10.3788/IRLA201746.0704001

Volume 46 Issue 7

Aug. 2017

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Cai Honghua, Nie Wansheng, Wu Rui, Su Lingyu, Hou Zhiyong. Establishment of narrow spectral band model parameters database for gas high temperature radiation characteristics[J]. Infrared and Laser Engineering, 2017, 46(7): 704001-0704001(8). doi: 10.3788/IRLA201746.0704001

Citation:

Cai Honghua, Nie Wansheng, Wu Rui, Su Lingyu, Hou Zhiyong. Establishment of narrow spectral band model parameters database for gas high temperature radiation characteristics[J]. Infrared and Laser Engineering, 2017, 46(7): 704001-0704001(8). doi: 10.3788/IRLA201746.0704001

Establishment of narrow spectral band model parameters database for gas high temperature radiation characteristics

doi: 10.3788/IRLA201746.0704001

1.
Department of Aerospace Equipment,The Academy of Equipment,Beijing 101416,China

Received Date: 2016-11-09
Rev Recd Date: 2016-12-08
Publish Date: 2017-07-25

Abstract

The main radiation gas components are completely different in different propellant rocket engine exhaust plume, the gas spectral parameter database need to be built to quickly and accurately solve the infrared radiation characteristics of different propellant rocket exhaust plume using the spectral band model. A method of constructing the gas spectral parameter database and the program were proposed, based on the method and HITEMP2010, CO2 and H2O spectral parameter databases were establised with the wave number interval 5 cm-1 and the temperature interval 100 K; the model and the program were verified to be correct through comparing the calculated absorption coefficient distribution with the experimental measurements and comparing the calculated transmittance distribution with that calculated using the line-by-line method. Based on that, CO, OH, NO and NO2 spectral parameter databases were established based on HITEMP2010 and HITRAN 2012, and the transmittance distributions on different temperatures and different optical strokes were comparatively analyzed combined with the line-by-line method.
- infrared radiation characteristics,
- band model parameters,
- spectroscopic database,
- HITEMP2010,
- HITRAN2012

References

[1]	Morizumi S J, Carpenter M J. Thermal radiation from the exhaust plume of an aluminized composite propellant rocket[J]. Journal of Spacecraft and Rocket, 1964, 1(4):501-507.
[2]	Xu Nanrong. Numerical computation on infrared plume radiation[J]. Acta Aerospace et Astronautica Sinica, 1995, 16(6):647-653. (in Chinese)徐南荣. 喷气流红外辐射场的数值计算[J]. 航空学报,1995, 16(6):647-653.
[3]	Zhang Haixing, Zhang Jianqi, Yang Wei. Theoretical calculation of the IR radiation of an aeroplane[J]. Journal of Xidian University, 1997, 24(1):78-81. (in Chinese)张海兴, 张建奇, 杨威. 飞机红外辐射的理论计算[J]. 西安电子科技大学学报, 1997, 24(1):78-81.
[4]	Mei Fei, Jiang Yong, Chen Shiguo, et al. Experimental verification and line by line prediction model of gas absorption[J]. Acta Optica Sinica, 2012, 32(3):0330002.(in Chinese)梅飞, 江勇, 陈世国, 等. 一种气体吸收的逐线计算模型及其实验验证[J]. 光学学报, 2012, 32(3):0330002.
[5]	Wang Darui, Zhang Nan, Ge Minghe. Calculation method on infrared of liquid rocket exhaust plume[J]. Missiles and Space Vehicles, 2015, 1(1):69-73. (in Chinese)王大锐, 张楠, 葛明和. 液体火箭发动机尾焰红外辐射计算方法[J]. 导弹与航天运载技术, 2015, 1(1):69-73.
[6]	Dong Shikui, Yu Qizheng, Liu Linhua, et al. A new method of calculating high temperature radiative property parameters of narrow-band model for CO2[J]. Journal of Engineering Thermophysics, 2001, 22(S):177-180.(in Chinese)董士奎, 余其铮, 刘林华, 等. 一种新的CO2高温辐射特性窄谱带模型参数计算方法[J]. 工程热物理学报, 2001, 22(S):177-180.
[7]	Dong Shikui, Yu Qizheng, Tan Heping, et al. Narrow band model parameters of high temperature radiation for carbon dioxide of combustion products[J]. Journal of Aerospace Power, 2001, 16(4):355-359. (in Chinese)董士奎, 余其铮, 谈和平, 等. 燃烧产物二氧化碳高温辐射的窄谱带模型参数[J]. 航空动力学报, 2001, 16(4):355-359.
[8]	Dong Shikui, Yu Qizheng, Tan Heping, et al. Infrared radiation band model parameters of water vapor in 300-3000 K[J]. Thermal Power Engineering, 2001, 16(91):33-38. (in Chinese)董士奎, 余其铮, 谈和平, 等. 300~3000 K水蒸气红外辐射谱带模型参数[J]. 热能动力工程, 2001, 16(91):33-38.
[9]	Chen Shiguo, Chen Lihai, Mo Dongla, et al. Construction of Malkmus statistical narrow spectral band model parameters database on HITEMP2010[J]. Infrared and Laser Engineering, 2015, 44(8):2327-2333. (in Chinese)陈世国, 陈立海, 莫冬腊, 等. 利用HITEMP2010的Malkmus窄谱带模型参数库构建研究[J]. 红外与激光工程, 2015, 44(8):2327-2333.
[10]	Saufiani A, Taine J. High temperature gas radiative property parameters of statistical narrow-band model for H2O, CO2 and CO, and correlated-K model for H2O and CO2[J]. Journal of Heat Mass Transfer, 1997, 40(4):987-991.
[11]	Qiao Ye, Nie Wansheng, Feng Songjiang, et al. Numerical research on influence exerted by afterburning on flow field and radiation characteristics of LH2/LOX rocket engine[J]. Missiles and Space Vehicles, 2016, 2(2):22-26. (in Chinese)乔野, 聂万胜, 丰松江, 等. 复燃对氢氧火箭发动机尾焰流场及辐射特性影响数值研究[J]. 导弹与航天运载技术, 2016, 2(2):22-26.
[12]	Liu Zunyang, Shao Li, Wang Yafu, et al. Influence on afterburning on infrared radiation of solid rocket exhaust plume[J]. Acta Optica Sinica, 2013, 33(6):0604001.(in Chinese)刘尊洋, 邵立, 汪亚夫, 等. 复燃对固体火箭尾焰红外辐射特性的影响[J]. 光学学报, 2013, 33(6):0604001.
[13]	Alexeenko A A, Gimelshein N E, Levin D A. Modeling of flow and radiation in the Atlas plume[J]. Journal of Thermophysics and Heat Transfer, 2002, 16(1):50-57.
[14]	Garrison M B, Ozawa T, Levin D A. An improved CO2, H2O, and soot infrared radiation models for high temperature flows[C]//36th AIAA Plasmadynamics and Lasers Conference, 2005:AIAA 2005-4777.
[15]	Young S J. Nonisothermal band model theory[J]. Journal of Quantitative Spectroscopy Radiative Transfer, 1976, 18:1-28.
[16]	Gamache R R, Kennedy S, Hawkins R, et al. Total internal partition sums for molecules in the terrestrial atmosphere[J]. Journal of Molecular Structure, 2000, 517-518:407-425.
[17]	Ludwig C B, Malkmus W, Reardon J E, et al. Handbook of infrared radiation from combustion gases. NASA SP-3080[Z]. 1973.

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通讯作者: 陈斌, bchen63@163.com

1.
沈阳化工大学材料科学与工程学院沈阳 110142

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Establishment of narrow spectral band model parameters database for gas high temperature radiation characteristics

1. Department of Aerospace Equipment,The Academy of Equipment,Beijing 101416,China

Received Date: 2016-11-09

Rev Recd Date: 2016-12-08

Publish Date: 2017-07-25

Key words:

Abstract: The main radiation gas components are completely different in different propellant rocket engine exhaust plume, the gas spectral parameter database need to be built to quickly and accurately solve the infrared radiation characteristics of different propellant rocket exhaust plume using the spectral band model. A method of constructing the gas spectral parameter database and the program were proposed, based on the method and HITEMP2010, CO2 and H2O spectral parameter databases were establised with the wave number interval 5 cm-1 and the temperature interval 100 K; the model and the program were verified to be correct through comparing the calculated absorption coefficient distribution with the experimental measurements and comparing the calculated transmittance distribution with that calculated using the line-by-line method. Based on that, CO, OH, NO and NO2 spectral parameter databases were established based on HITEMP2010 and HITRAN 2012, and the transmittance distributions on different temperatures and different optical strokes were comparatively analyzed combined with the line-by-line method.

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Reference (17)

[1]	Morizumi S J, Carpenter M J. Thermal radiation from the exhaust plume of an aluminized composite propellant rocket[J]. Journal of Spacecraft and Rocket, 1964, 1(4):501-507.
[2]	Xu Nanrong. Numerical computation on infrared plume radiation[J]. Acta Aerospace et Astronautica Sinica, 1995, 16(6):647-653. (in Chinese)徐南荣. 喷气流红外辐射场的数值计算[J]. 航空学报,1995, 16(6):647-653.
[3]	Zhang Haixing, Zhang Jianqi, Yang Wei. Theoretical calculation of the IR radiation of an aeroplane[J]. Journal of Xidian University, 1997, 24(1):78-81. (in Chinese)张海兴, 张建奇, 杨威. 飞机红外辐射的理论计算[J]. 西安电子科技大学学报, 1997, 24(1):78-81.
[4]	Mei Fei, Jiang Yong, Chen Shiguo, et al. Experimental verification and line by line prediction model of gas absorption[J]. Acta Optica Sinica, 2012, 32(3):0330002.(in Chinese)梅飞, 江勇, 陈世国, 等. 一种气体吸收的逐线计算模型及其实验验证[J]. 光学学报, 2012, 32(3):0330002.
[5]	Wang Darui, Zhang Nan, Ge Minghe. Calculation method on infrared of liquid rocket exhaust plume[J]. Missiles and Space Vehicles, 2015, 1(1):69-73. (in Chinese)王大锐, 张楠, 葛明和. 液体火箭发动机尾焰红外辐射计算方法[J]. 导弹与航天运载技术, 2015, 1(1):69-73.
[6]	Dong Shikui, Yu Qizheng, Liu Linhua, et al. A new method of calculating high temperature radiative property parameters of narrow-band model for CO2[J]. Journal of Engineering Thermophysics, 2001, 22(S):177-180.(in Chinese)董士奎, 余其铮, 刘林华, 等. 一种新的CO2高温辐射特性窄谱带模型参数计算方法[J]. 工程热物理学报, 2001, 22(S):177-180.
[7]	Dong Shikui, Yu Qizheng, Tan Heping, et al. Narrow band model parameters of high temperature radiation for carbon dioxide of combustion products[J]. Journal of Aerospace Power, 2001, 16(4):355-359. (in Chinese)董士奎, 余其铮, 谈和平, 等. 燃烧产物二氧化碳高温辐射的窄谱带模型参数[J]. 航空动力学报, 2001, 16(4):355-359.
[8]	Dong Shikui, Yu Qizheng, Tan Heping, et al. Infrared radiation band model parameters of water vapor in 300-3000 K[J]. Thermal Power Engineering, 2001, 16(91):33-38. (in Chinese)董士奎, 余其铮, 谈和平, 等. 300~3000 K水蒸气红外辐射谱带模型参数[J]. 热能动力工程, 2001, 16(91):33-38.
[9]	Chen Shiguo, Chen Lihai, Mo Dongla, et al. Construction of Malkmus statistical narrow spectral band model parameters database on HITEMP2010[J]. Infrared and Laser Engineering, 2015, 44(8):2327-2333. (in Chinese)陈世国, 陈立海, 莫冬腊, 等. 利用HITEMP2010的Malkmus窄谱带模型参数库构建研究[J]. 红外与激光工程, 2015, 44(8):2327-2333.
[10]	Saufiani A, Taine J. High temperature gas radiative property parameters of statistical narrow-band model for H2O, CO2 and CO, and correlated-K model for H2O and CO2[J]. Journal of Heat Mass Transfer, 1997, 40(4):987-991.
[11]	Qiao Ye, Nie Wansheng, Feng Songjiang, et al. Numerical research on influence exerted by afterburning on flow field and radiation characteristics of LH2/LOX rocket engine[J]. Missiles and Space Vehicles, 2016, 2(2):22-26. (in Chinese)乔野, 聂万胜, 丰松江, 等. 复燃对氢氧火箭发动机尾焰流场及辐射特性影响数值研究[J]. 导弹与航天运载技术, 2016, 2(2):22-26.
[12]	Liu Zunyang, Shao Li, Wang Yafu, et al. Influence on afterburning on infrared radiation of solid rocket exhaust plume[J]. Acta Optica Sinica, 2013, 33(6):0604001.(in Chinese)刘尊洋, 邵立, 汪亚夫, 等. 复燃对固体火箭尾焰红外辐射特性的影响[J]. 光学学报, 2013, 33(6):0604001.
[13]	Alexeenko A A, Gimelshein N E, Levin D A. Modeling of flow and radiation in the Atlas plume[J]. Journal of Thermophysics and Heat Transfer, 2002, 16(1):50-57.
[14]	Garrison M B, Ozawa T, Levin D A. An improved CO2, H2O, and soot infrared radiation models for high temperature flows[C]//36th AIAA Plasmadynamics and Lasers Conference, 2005:AIAA 2005-4777.
[15]	Young S J. Nonisothermal band model theory[J]. Journal of Quantitative Spectroscopy Radiative Transfer, 1976, 18:1-28.
[16]	Gamache R R, Kennedy S, Hawkins R, et al. Total internal partition sums for molecules in the terrestrial atmosphere[J]. Journal of Molecular Structure, 2000, 517-518:407-425.
[17]	Ludwig C B, Malkmus W, Reardon J E, et al. Handbook of infrared radiation from combustion gases. NASA SP-3080[Z]. 1973.

Establishment of narrow spectral band model parameters database for gas high temperature radiation characteristics

doi: 10.3788/IRLA201746.0704001

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References

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通讯作者: 陈斌, bchen63@163.com

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