Return to search

Unsteady aerodynamic response of the rotor blades of an axial flow compressor operating under conditions of circumferential inlet distortions and rotating stall

No description available.

1. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.348216

Identifer	oai:union.ndltd.org:bl.uk/oai:ethos.bl.uk:348216
Date	January 1983
Creators	Ozcanli, S. C.
Publisher	Cranfield University
Source Sets	Ethos UK
Detected Language	English
Type	Electronic Thesis or Dissertation