The excitation of acoustic resonances in an axial flow compressor stage by vortex shedding from aerofoil section blading
In recent years continuing development of the axial flow compressor for use in the aero-engine has increased its susceptibility to unsteady flow phenomena which can cause severe blade vibration. A source which has emerged and become of considerable importance is excitation by acoustic resonances. An...
| Main Author: | |
|---|---|
| Published: |
Swansea University
1986
|
| Subjects: | |
| Online Access: | http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.636209 |