Effects of transverse ribs on pressure recovery in two-dimensional subsonic diffusers
- 16 August 1972
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Straight Channel Diffuser Performance at High Inlet Mach NumbersJournal of Basic Engineering, 1969