Multi-dimensional formulation of CSCM - An upwind flux difference eigenvector split method for the compressible Navier-Stokes equations

Euler equations - Implicit schemes and boundary conditions

Sukumar Chakravarthy · AIAA Journal · 1983 · 99 citations

Natural Sciences, Aerospace Engineering, Mathematics +17

Two-Dimensional Inlet Simulation Using a Diagonal Implicit Algorithm

D. CHAUSSEE, Thomas H. Pulliam · AIAA Journal · 1981 · 55 citations

Engineering, Aerospace Engineering, Computational Engineering +15

Conservative supra-characteristics method for splitting the hyperbolic systems of gasdynamics with computed boundaries for real and perfect gases

C. LOMBARD, Joseph Oliger, James Yang et al. · 3rd Joint Thermophysics, Fluids, Plasma and Heat Transfer Conference · 1982 · 19 citations

Engineering, Mechanical Engineering, Physics +14

Numerical experiments with the split-flux-vector form of the Euler equations

J. DEESE · 21st Aerospace Sciences Meeting · 1983 · 15 citations

Engineering, Mathematics, Mechanical Engineering +17

A characteristic flux difference splitting for the hyperbolic conservation laws of inviscid gasdynamics

James Yang, C. LOMBARD, D. Bershader · 21st Aerospace Sciences Meeting · 1983 · 13 citations

Natural Sciences, Physics, Computational Fluid Dynamics +8