Pointwise non-oscillatory shock capturing scheme
Abstract
Representing a numerical flux of the pointwise scheme as pointwise value at the cell boundary, new pointwise non-oscillatory shock capturing scheme was constructed. The present scheme was examined for unsteady/steady supersonic flow problem. The results showed that the present scheme is quite useful particularly for the strongly viscous-inviscid interacted flows with upstream feedback.
- Publication:
-
6th National Symposium on Computational Fluid Dynamics
- Pub Date:
- September 1993
- Bibcode:
- 1993cfd..proc..535I
- Keywords:
-
- Computerized Simulation;
- Flow Distribution;
- Numerical Analysis;
- Numerical Flow Visualization;
- Steady Flow;
- Supersonic Flow;
- Unsteady Flow;
- Algorithms;
- Computational Fluid Dynamics;
- Mach Number;
- Mach Reflection;
- Mathematical Models;
- Nonoscillatory Action;
- Nozzle Flow;
- Pressure Distribution;
- Shock Waves;
- Supersonic Combustion Ramjet Engines;
- Fluid Mechanics and Heat Transfer