Film cooling of gas turbine blades
An experimental apparatus was designed and built to study the film cooling effectiveness from a single row of holes at various angles and hole spacings, using a foreign gas technique. Mixtures of Freon 12 and air were injected into an air mainstream to give a range of density ratios encompassing the...
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University of Nottingham
1976
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| Online Access: | http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.455803 |