Infrared and Laser Engineering, Volume. 54, Issue 3, 20240398(2025)
Numerical simulation of infrared radiation characteristics of high-speed aircraft’s stage separation flow field
[12] [12] DONG W. Numerical simulation analysis of thermalchemical noneequilibrium effects at highspeed flows[D]. Beijing: Beijing University of Aeronautics Astronautics, 1996. (in Chinese)
[13] [13] DESPIRITO J. Effects of turbulence model on prediction of hotgas lateral jet interaction in a supersonic crossflow, AIAA20151923[R]. Reston: AIAA, 2015.
[14] [14] SURZHIKOV S T, SHANG J S. Kiic models analysis f superbital aerophsics, AIAA20081278 [R]. Reston: AIAA, 2008.
[15] [15] PARK C, JAFFE R L, PARTRIDGE H. Chemicalkiic parameters of hyperbolic Earth entries, AIAA00021 [R]. Reston: AIAA, 2000.
[18] [18] ZHAO H. Parallel numerical study of whole scramjet engine[D]. Mianyang: China Aerodynamics Research Development Center, 2005. (in Chinese)
[19] [19] LUDWIG C B, MALKMUS W, REARDON J, et al. Hbook of infrared radiation from combustion gases, NASASP3080[R]. Alabama: NASA, 1973.
[20] [20] DENVIR A, LESSIN A, LEV M, et al. Comparison of calculated measured radiation from a rocket mot plume, AIAA20010358[R]. Reston: AIAA, 2001.
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Yang’aoxiao FU, Mingsong DING, Qingzong LIU, Peng LI, Weizhong DONG, Tiesuo GAO, Tao JIANG. Numerical simulation of infrared radiation characteristics of high-speed aircraft’s stage separation flow field[J]. Infrared and Laser Engineering, 2025, 54(3): 20240398
Category: Infrared
Received: Sep. 10, 2024
Accepted: --
Published Online: Apr. 8, 2025
The Author Email: Tao JIANG (fengqiaoren999@163.com)