Supersonic through-flow fan design
- 29 June 1987
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Development of an explicit multigrid algorithm for quasi-three-dimensional viscous flows in turbomachineryPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- The Supersonic Axial Inlet Component in a CompressorPublished by ASME International ,1975