[1] Roe PL (1981) Approximate Riemann solvers, parameter vectors, and difference schemes. J Comput Phys 43(2): 357-372.
[2] Toro EF, Spruce M, Speares W (1994) Restoration of the contact surface in the HLL-Riemann solver. Shock Waves 4(1): 25-34.
[3] Peery K, Imlay S (1988) Blunt-body flow simulations. In 24th Joint Propulsion Conference.
[4] Van Leer B (1997) Flux-vector splitting for the Euler equation. In Upwind and High-Resolution Schemes (pp. 80-89). Springer, Berlin, Heidelberg.
[5] Steger JL, Warming RF (1981) Flux vector splitting of the inviscidgasdynamic equations with application to finite-difference methods. J Comput Phys 40(2): 263-293.
[6] Liou MS, Steffen JrCJ (1993) A new flux splittingscheme. J Comput Phys 107(1): 23-39.
[7] Meng-Sing L (1996) A sequel to AUSM: AUSM+. Journal of Computational Physics 129(1): 12-16.
[8] Kim KH, Kim C, Rho OH (2001) Methods for the accurate computations of hypersonic flows: I.AUSMPW+ scheme. J Comput Phys 174(1): 38-80.
[8] Kim KH, Kim C, Rho OH (2001) Methods for the accurate computations of hypersonic flows: I.AUSMPW+ scheme. J Comput Phys 174(1): 38-80.
[9] Liou MS (2006) A sequel to AUSM, Part II: AUSM+-up for all speeds. J Comput Phys 214(1): 137-170.
[10] Shima E, Kitamura K (2011) Parameter-free simple low-dissipation AUSM-family scheme for all speeds. AIAA J 49(8): 1693-1709.
[11] Chakravarthy K, Chakraborty D (2014) Modified SLAU2 scheme with enhanced shock stability. Comput Fluids 100: 176-184.
[12] Chen SS, Yan C, Lin BX, Liu LY, Yu J (2018) Affordable shock-stable item for Godunov-type schemes against carbuncle phenomenon. J Comput Phys 373: 662-672.
[13] Shima E, Kitamura K (2009) On new simple low-dissipation scheme of AUSM-family for all speeds. In 47th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition.
[14] Shima E, Kitamura K (2009) On AUSM-family scheme for all speeds with shock detection for carbuncle-fix. In 19th AIAA Computational Fluid Dynamics.
[15] Zhang F, Liu J, Chen B, Zhong W (2017) A robust low‐dissipation AUSM‐family scheme for numericalshock stability on unstructured grids. Int J Numer Methods Fluids 84(3): 135-151.
[16] Singh R, Holmes G (2012) Evaluation of an artificial dissipation and AUSM based flux formulation: AD-AUSM. In 42nd AIAA Fluid Dynamics Conference and Exhibit.
[17] Guo S, Tao WQ (2018) A hybrid flux splitting method for compressible flow. Numer Heat Tr B-Fund 73(1): 33-47.
[18] Chen SS, Cai FJ, Xue HC, Wang N, Yan C (2020) An improved AUSM-family scheme with robustness and accuracy for all Mach number flows. Appl Math Model 77: 1065-1081.
[19] Chen SS, Yan C, Lin BX, Liu LY, Yu J (2018) Affordable shock-stable item for Godunov-type schemes against carbuncle phenomenon. J Comput Phys 373: 662-672.
[20] Kim KH, Kim C, Rho OH (2001) Methods for the accurate computations of hypersonic flows: I.AUSMPW+ scheme. J Comput Phys 174(1): 38-80.
[21] Tian Z, Wang G, Zhang F, Zhang H (2020) A third-order compact nonlinear scheme for compressible flow simulations. Int J Numer Methods Fluids.
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