Airfoil Design for High Tip Speed Compressors
- 1 November 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 11 (11) , 682-689
- https://doi.org/10.2514/3.60404
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Comparison of Performance of Supersonic Blading in Cascade and in Compressor RotorsJournal of Engineering for Power, 1971
- Shock Losses in Transonic Compressor Blade RowsJournal of Engineering for Power, 1961