Effects of inflow distortion profiles on fan tone noise calculated using a 3-D theory
- 12 March 1979
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Modal propagation angles in a cylindrical duct with flow and their relation to sound radiationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Three-dimensional effects on pure tone fan noise due to inflow distortionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Summary of forward velocity effects on fan noisePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Inlet turbulence and fan noise measured in an anechoic wind tunnel and statically with an inlet flow control devicePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Three-dimensional analysis of blade force and sound generation for an annular cascade in distorted flowsJournal of Sound and Vibration, 1977