A mixed explicit-implicit antidiffusive method of Navier-Stokes equations for supersonic and hypersonic separated flows
Abstract
A mixed explicit/implicit scheme based on an antidiffusive method is used to solve the Navier-Stokes equations for the supersonic and hypersonic separated flows. The computations are performed for laminar and turbulent flows compared with the results of numerically computing NS equations and these results of the experiments. The computations show that the numerical scheme is satisfactory.
- Publication:
-
NASA STI/Recon Technical Report N
- Pub Date:
- April 1984
- Bibcode:
- 1984STIN...8428005C
- Keywords:
-
- Flow Distribution;
- Hypersonic Flow;
- Navier-Stokes Equation;
- Separated Flow;
- Supersonic Flow;
- Boundary Layer Separation;
- Finite Difference Theory;
- Hypersonics;
- Multiphase Flow;
- Procedures;
- Fluid Mechanics and Heat Transfer