| Citation: | Zhao Rui, Yan Chao, Yu Jianet al. New kind Baldwin-Lomax turbulence model under the limit of entropy[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (2): 175-179,190. (in Chinese) | 
	                | [1] | 
					 Baldwin B S, Lomax H. Thin layer approximation and algebraic model for seperated turbulent flows[R]. AIAA-78-257, 1978 
					
					 | 
			
| [2] | 
					 Degani D, Schiff L B. Computation of supersonic viscous flows around pointed bodies at large incidence[R]. AIAA-83-0034, 1983 
					
					 | 
			
| [3] | 
					 Panaras A G, Steger J L. A thin-layer solution of the flow about a prolate spheroid [J]. Z Flugwiss, 1988(12):173-180 
					
					 | 
			
| [4] | 
					 Panaras A G. Algebraic turbulence modeling for swept shock-wave/turbulent boundary-layer interactions [J]. AIAA Journal, 1997,35(2):456-463 
					
					 | 
			
| [5] | 
					 Shang J S, Hankey W L, Jr. Numerical solution for supersonic turbulent flow over a compression ramp[J]. AIAA Journal, 1975,13(10):1368-1374 
					
					 | 
			
| [6] | 
					 Wilcox D C. Reassessment of the scale determining equation for advanced turbulence models[J]. AIAA Journal, 1988, 26(11): 1299-1310 
					
					 | 
			
| [7] | 
					 Gao H, Fu D X, Ma Y W, et al. Direct numerical simulation of supersonic turbulent boundary layer flow[J]. Chinese Physics Letters, 2005, 22(7): 1709-1712 
					
					 | 
			
| [8] | 
					 Settles G S, Dodson L J. Hypersonic shock/boundary-layer interaction database[R]. NASA-CR-177577, 1991 
					
					 | 
			
| [9] | 
					 Visbal M, Knight D. The Baldwin-Lomax turbulence model for two-dimensional shock-wave/boundary-layer Interactions[J]. AIAA Journal, 1984,22(7):921-928 
					
					 | 
			
| [10] | 
					 Forsythe R, Hoffmann A, Damevin M. An assessment of several turbulence models for supersonic compression ramp flow[R]. AIAA 98-2648, 1998 
					
					 | 
			
| [11] | 
					 Knight D. RTO WG 10: test cases for CFD validation of hypersonic flight[R]. AIAA 2002-0433, 2002 
					
					 | 
			
| [12] | 
					 Knight D, ran H, Panaras A, et al. RTO WG 10: CFD validation for shock wave turbulent boundary layer interactions[R]. AIAA 2002-0437, 2002 
					
					 |