Noise generation by a rotating blade row in an infinite annulus
- 21 June 1971
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Sound transmission and generation in ducts with flowJournal of Sound and Vibration, 1971
- Three-dimensional vortex theory for axial compressor blade rows at subsonic and transonic speedsAIAA Journal, 1970
- Axial Flow Compressor Noise StudiesSAE International Journal of Advances and Current Practices in Mobility, 1962
- On the Vortex Theory of the Screw PropellerJournal of the Aeronautical Sciences, 1937