Numerical analysis of supersonic flow through oscillating cascade sections by using a deforming grid
- 12 July 1989
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Explicit multigrid algorithm for quasi-three-dimensional viscous flows in turbomachineryJournal of Propulsion and Power, 1987