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Heat transfer near the entrance to a film cooling hole in a gas turbine blade

No description available.
Identiferoai:union.ndltd.org:bl.uk/oai:ethos.bl.uk:329915
Date January 1989
CreatorsByerley, Aaron R.
PublisherUniversity of Oxford
Source SetsEthos UK
Detected LanguageEnglish
TypeElectronic Thesis or Dissertation

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