Small disturbances in turbomachine annuli with swirl
- 1 June 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 15 (6) , 794-803
- https://doi.org/10.2514/3.7370
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- The effects of trailing vorticity on the flow through highly loaded cascadesJournal of Fluid Mechanics, 1976
- Noise generation by a rotating blade row in an infinite annulusPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1971
- Three-dimensional vortex theory for axial compressor blade rows at subsonic and transonic speedsAIAA Journal, 1970
- A Three Dimensional Theory of Axial Compressor Blade Rows - Application in Subsonic and Supersonic FlowsJournal of the Aerospace Sciences, 1958