Development of an explicit multigrid algorithm for quasi-three-dimensional viscous flows in turbomachinery
- 6 January 1986
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 14 references indexed in Scilit:
- Application of Runge Kutta time marching scheme for the computation of transonic flows in turbomachinesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Transonic Blade to Blade Calculations in an Axial, Radial or Mixed Flow Cascade Equipped With Splitter BladesPublished by ASME International ,1985
- Analysis of inviscid and viscous flows in cascades with an explicit multiple-grid algorithmPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- A Rapid Blade-to-Blade Solution for Use in Turbomachinery DesignJournal of Engineering for Gas Turbines and Power, 1984
- Multigrid solution of the Euler equations for aircraft configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Solution of Plane Cascade Flow Using Improved Surface Singularity MethodsJournal of Engineering for Power, 1982
- Full Potential Solution of Transonic Quasi-Three-Dimensional Flow Through a Cascade Using Artificial CompressibilityJournal of Engineering for Power, 1982
- A multiple grid scheme for solving the Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Second-Order-Accurate Calculation of Transonic Flow over Turbomachinery CascadesAIAA Journal, 1979
- The effect of viscosity in hypervelocity impact crateringPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969