1 한상훈, "압축성 코드에서 예조건화 코드로의 이전" 한국항공우주학회 35 (35): 183-195, 2007
2 김태우, "압축성 유동 해석을 위한 압력 기반 해석자의 개선된 알고리즘 개발" 한국전산유체공학회 22 (22): 28-35, 2017
3 Lax, P.D., "Weak solutions of nonlinear hyperbolic equations and their numerical computation" 7 : 159-193, 1954
4 Cuffel, R.F., "Transonic Flowfield in a Supersonic Nozzle with Small Throat Radius of Curvature" 7 (7): 1364-1366, 1969
5 Choi, Y., "The appilcation of Preconditioning in Viscous Flows" 107 : 207-223, 1993
6 Graves, E.B., "Stability And Control Characteristics At Mach Numbers From 0.20 To 4.63 Of A Cruciform Air-To-Air Missile With Triangular Canard Controls And A Trapezoidal Wing" NASA Technical Memorandum 1974
7 Emans, M., "SIMPLE-H: a finite-volume pressure-enthalpy coupling scheme for flows with variable density" 69 (69): 206-, 2012
8 Patankar, J., "Numerical heat transfer and fluid flow" CRC press 1980
9 Shu, C.-W., "Numerical experiments on the accuracy of ENO and modified ENO schemes" 5 (5): 127-149, 1990
10 Kim, S.D., "Comparison of Low-Mach number fixing methods for Roe scheme" 2012
1 한상훈, "압축성 코드에서 예조건화 코드로의 이전" 한국항공우주학회 35 (35): 183-195, 2007
2 김태우, "압축성 유동 해석을 위한 압력 기반 해석자의 개선된 알고리즘 개발" 한국전산유체공학회 22 (22): 28-35, 2017
3 Lax, P.D., "Weak solutions of nonlinear hyperbolic equations and their numerical computation" 7 : 159-193, 1954
4 Cuffel, R.F., "Transonic Flowfield in a Supersonic Nozzle with Small Throat Radius of Curvature" 7 (7): 1364-1366, 1969
5 Choi, Y., "The appilcation of Preconditioning in Viscous Flows" 107 : 207-223, 1993
6 Graves, E.B., "Stability And Control Characteristics At Mach Numbers From 0.20 To 4.63 Of A Cruciform Air-To-Air Missile With Triangular Canard Controls And A Trapezoidal Wing" NASA Technical Memorandum 1974
7 Emans, M., "SIMPLE-H: a finite-volume pressure-enthalpy coupling scheme for flows with variable density" 69 (69): 206-, 2012
8 Patankar, J., "Numerical heat transfer and fluid flow" CRC press 1980
9 Shu, C.-W., "Numerical experiments on the accuracy of ENO and modified ENO schemes" 5 (5): 127-149, 1990
10 Kim, S.D., "Comparison of Low-Mach number fixing methods for Roe scheme" 2012
11 Mangani, L., "An OpenFOAM pressure-based coupled CFD solver for turbulent and compressible flows in turbomachinery applications" 69 (69): 413-, 2016
12 Wee, H.C., "Aerodynamic Analysis Of A Canard Missile Configuration Using Ansys-Cfx" Naval Postgraduate School 2011
13 Kraposhin, M., "Adaptation of Kurganov-Tadmor Numerical Scheme For Applying in Combination With the PISO Method in Numerical Simulation of Flows in a Wide Range of Mach Numbers" 66 : 43-52, 2015
14 Sod, G.A., "A survey of several finite difference methods for systems of non-linear hyperbolic conservation laws" 27 (27): 1-159, 1978
15 Emans, M., "A novel SIMPLE-based pressure-enthalpy coupling scheme for engine flow problems" 17 (17): 1-, 2012
16 Rieper, F., "A low-Mach number fix for Roe’s approximate Riemann solver" 230 : 5263-5287, 2011
17 Darwish, M., "A Fully Coupled Navier-Stokes Solver for Fluid Flow at All Speeds" 65 (65): 410-, 2014