The effects of trailing edge coolant on trailing edge losses
This thesis reports on an experimental investigation into the trailing edge pressure and losses of a symmetrical isolated aerodynamic body under transonic flow conditions. Tests were made in the 4" x 4" transonic wind tunnel at the University of Liverpool. The test programme included bleed...
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University of Liverpool
1980
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| Online Access: | http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.539104 |