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The effect of upstream boundary layer state on the shock interaction at a compression corner

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1. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.257332

Identifer	oai:union.ndltd.org:bl.uk/oai:ethos.bl.uk:257332
Date	January 1980
Creators	Hayakawa, K.
Publisher	University of Cambridge
Source Sets	Ethos UK
Detected Language	English
Type	Electronic Thesis or Dissertation