Pages that link to "Item:Q1069378"

The following pages link to Computation of steady supersonic flows by a flux-difference/splitting method (Q1069378):

Displaying 17 items.

• Complex conservative difference schemes for computing supersonic flows past simple aerodynamic forms (Q266099) (← links)
• Steady supersonic flow-field predictions using proper orthogonal decomposition technique (Q435365) (← links)
• Application of a direct method for solving the Boltzmann equation in supersonic flow computation (Q518552) (← links)
• Numerical experiments with nonoscillatory schemes using Eulerian and new Lagrangian formulations (Q686878) (← links)
• A new Lagrangian method for steady supersonic flow computation. I: Godunov scheme (Q912720) (← links)
• The behavior of flux difference splitting schemes near slowly moving shock waves (Q913602) (← links)
• A finite difference scheme for steady, supersonic, two-dimensional, compressible flow of real gases (Q1205903) (← links)
• On flux-extrapolation at supersonic outflow boundaries (Q1294612) (← links)
• A difference scheme for quasicharacteristics and its use to calculate supersonic gas flow (Q1309065) (← links)
• A numerical method for solving the three-dimensional parabolized Navier-Stokes equations (Q1373146) (← links)
• A high-order streamline Godunov scheme for steady supersonic flow computation. (Q1578653) (← links)
• A second-order finite-volume scheme for Euler equations: kinetic energy preserving and staggering effects (Q1704775) (← links)
• On the irrotational approximation to steady supersonic flow (Q2369860) (← links)
• Evaluation of non-oscillatory schemes based on LED principle for supersonic flow computations (Q2575206) (← links)
• An adjoint method for the calculation of remote sensitivities in supersonic flow (Q3551545) (← links)
• Computation of non-equilibrium hypersonic flow with artificially upstream flux vector splitting (AUFS) schemes (Q3551629) (← links)
• (Q3610075) (← links)