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Zare Shahneh, Abolghasern
It is well known that in transonic flows, shQtk waves are fonned over the wings of aircraft. Depending on the strength of the shock wave and the state of the boundary layer, a region of boundary layer separation can occur downstream of the shock. Thi
Externí odkaz:
http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.485561
