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

No description available.
Identiferoai:union.ndltd.org:bl.uk/oai:ethos.bl.uk:344070
Date January 1998
CreatorsKais, G.
PublisherUniversity of Sussex
Source SetsEthos UK
Detected LanguageEnglish
TypeElectronic Thesis or Dissertation

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