[1] | Gokhale S S, Kumar V R.null Numerical computations of supersonic inlet flow [J]. Int J Numer Meth Fluids.2001,36:597- | [2] | Jong Y O, Fuhua Ma, Shih-Yang H,�� et al.�� Interactions between shock and acoustic waves in a supersonic inlet diffuser [J] Journal of Propulsion and Power, 2005,21(3):486~495 | [3] | Weiss J M, Smith W A. Preconditioning applied to variable and constant density flows [J] AIAA Journal, 1995, 33(11):2050~2057 | [4] | Chen K H, Shuen J S. Three-dimensional coupled implicit methods for spray combustion flows at all speeds . AIAA 94-3047, 1994 | [5] | Edwards J R, Liou M S. Low-diffusion flux-splitting methods for flows at all speeds [J] AIAA Journal, 1998, 36(9):1610~1617 | [6] | Reed C L. Low speed preconditioning applied to compressible Navier-Stokes Equations . Texas:The Univ of Texas at Arlingtou, 1995 | [7] | ������,��Ī��,�����. �ǡ��硢�����ټ�����ѹ��������ֵ�����������о�[J] ������ѧѧ��,2001, 18(4):397~401 Zhao Xingyan, Su Moming, Miao Yongmiao. Numerical simulation of compressible and incompressible flows [J] Chinese Journal of Computational mechanics, 2001, 18(4):379~401 (in Chinese) | [8] | Ghia U, Ghia K N, Shin C T. High-resolutions for incompressible flow using the Navier-Stokes equations and a multigrid method [J] Journal of Computational Physics, 1982, 48(3):387~411 |
|