Radiative Heat Transfer in Film-Cooled Liquid Rocket Engine Nozzles
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[1] C. B. Ludwig,et al. Handbook of infrared radiation from combustion gases , 1973 .
[2] Ellis E. Whiting,et al. Modeling of nonequilibrium radiation phenomena - An assessment , 1996 .
[3] Do-Yeong Byeon,et al. A Numerical Study on the Combustion Characteristics in a Liquid Rocket Engine with Film Cooling Effect , 2003 .
[4] B. W. Webb,et al. A Spectral Line-Based Weighted-Sum-of-Gray-Gases Model for Arbitrary RTE Solvers , 1993 .
[5] T. F. Greenwood,et al. Space Shuttle base heating , 1984 .
[6] T. Fransson,et al. Improvement of the finite volume method for coupled flow and radiation calculations by the use of two grids and rotational periodic interfaces , 2001 .
[7] S. Tiwari,et al. Radiative heat transfer effects in chemically reacting nozzle flows , 1996 .
[8] F. Menter. Improved two-equation k-omega turbulence models for aerodynamic flows , 1992 .
[9] G. Hagemann,et al. Status of Low Separation Prediction in Rocket Nozzles. , 1998 .
[10] F. Menter. ZONAL TWO EQUATION k-w TURBULENCE MODELS FOR AERODYNAMIC FLOWS , 1993 .
[11] A. Hadjadj,et al. Numerical simulation of flow separation in rocket nozzle , 1997 .
[12] Fengshan Liu,et al. An assessment of real-gas modelling in 2D enclosures , 2000 .
[13] H. Nelson. Radiative Heating in Scramjet Combustors , 1997 .
[14] G. D. Raithby,et al. A Finite-Volume Method for Predicting a Radiant Heat Transfer in Enclosures With Participating Media , 1990 .