| Citation: | WU Zong-cheng, ZHU Zi-qiang, LI Jin, et al. Calculation and Analysis of the Flow Passing through a Multi-Element Wing[J]. Journal of Beijing University of Aeronautics and Astronautics, 2001, 27(3): 321-324. (in Chinese) | 
	                | 
					 [1] Pulliam T H, Steger J L. Implicit finite difference simulation of three dimensional compressible flow[J]. AIAA J, 1980, 18(2):159~167. [2] Baldwin B S, Lomax H. Thin layer approximation algebraic model for separated turbulent flows. AIAA 78-257,1978. [3] Jameson A, Schmidt W, Turkel E. Numerical solutions of the Euler equations by finite volume methods using Runge-Kutta time stepping schemes. AIAA 81-1259,1981. [4] Swanson R C, Turkel E. Artificial dissipation and central difference schemes for Euler and Navier-Stokes equations. AIAA 87-1107,1987. [5] Omar E, Zierten T, Hahn M, et al. Two dimensional wind-tunnel test of a NASA supercritical airfoil with various high lift systems. NASA CR-2215, 1974. [6] Dallmann U, Herberg Th, Gebing H, et al. Flow field diagnostics:Topological flow changes and spatio-temporal flow structure. AIAA 95-0791,1995. 
					
					 |