Boundary layer reattachment in hypersonic flow
The thesis describes a detailed experimental study of wedge and step separated flows performed in a hypersonic gun tunnel. Reattachment pressure and heat transfer distributions and pressures within the shear layer have been measured at Mach numbers of 8.2 and 9.7 using conical and contoured nozzle f...
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Imperial College London
1968
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| Online Access: | https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.623015 |