The aerodynamics of circulation control aerofoils
Two dimensional subsonic wind tunnel tests have been conducted on a 20% thickness: chord ratio circulation controlled elliptic aerofoil section equipped with forward and reverse blowing slots. Overall performance measurements were made over a range of trailing edge blowing momentum coefficients from...
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University of Bath
1981
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| Online Access: | https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.291934 |