Three-dimensional vortex theory for axial compressor blade rows at subsonic and transonic speeds
- 1 July 1970
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (7) , 1275-1283
- https://doi.org/10.2514/3.5885
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- The Transonic Flow Field of an Axial Compressor Blade RowJournal of the Aerospace Sciences, 1958
- A Three Dimensional Theory of Axial Compressor Blade Rows - Application in Subsonic and Supersonic FlowsJournal of the Aerospace Sciences, 1958
- On the Vortex Theory of the Screw PropellerJournal of the Aeronautical Sciences, 1937