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Heat transfer and fluid flow in the high pressure compressor drive cone cavity of an aeroengine

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1. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.344070

Identifer	oai:union.ndltd.org:bl.uk/oai:ethos.bl.uk:344070
Date	January 1998
Creators	Kais, G.
Publisher	University of Sussex
Source Sets	Ethos UK
Detected Language	English
Type	Electronic Thesis or Dissertation