The review of the IR radiation characteristic of exhaust plume of the liquid rocket engine

At present, there are various methods to compute the infrared radiation characteristics of exhaust plume of the liquid rocket engine. Though they are different in computational complexity. Their ideas and methods are alike. This paper focuses on the computation methods of exhaust plume’s flow field, spectral parameters and radiation transfer equation. Comparison, analysis and conclusion of these methods are presented. Furthermore, existing problems and improvements of them are proposed as well.

[1]  K. Case.  Transfer Problems and the Reciprocity Principle , 1957 .

[2]  A. A. Chursin,et al.  The 1997 spectroscopic GEISA databank , 1999 .

[3]  Direct simulation Monte-Carlo algorithms for the rocket exhaust plumes emissivity prediction , 2002 .

[4]  Zhou Xiao-dong.  The Progress of the Atmospheric Infrared Emission Models and Practical Codes , 2003 .

[5]  Ömer L. Gülder,et al.  Application of the statistical narrow-band correlated-k method to non-grey gas radiation in CO , 2001 .

[6]  Laurence S. Rothman,et al.  Reprint of: The HITRAN molecular spectroscopic database and HAWKS (HITRAN Atmospheric Workstation): 1996 edition , 1998 .

[7]  Laurence S. Rothman,et al.  The HITRAN molecular spectroscopic database and HAWKS (HITRAN atmospheric workstation) , 1998, Defense, Security, and Sensing.

[8]  Yang Chang-peng.  Numerical simulation of the infrared characteristic of missile exhaust plume , 2008 .

[9]  S. Dash,et al.  Computational models for the viscous/inviscid analysis of jet aircraft exhaust plumes. [predicting afterbody drag] , 1980 .

[10]  Cai Guobiao.  Study the Infrared Characteristics of the Solid Rocket Plume with DOM Method and the Influence of Altitude , 2007 .

[11]  Yurii L. Babikov,et al.  CDSD-1000: the high-temperature carbon dioxide spectroscopic databank and information system , 2004, Symposium on High-Resolution Molecular Spectroscopy.

[12]  Tang Xin-yi.  Building model of the plume released from the flying machine and simulation , 2007 .