The effect of nozzle exit geometry on the aerodynamic performance of bypass flow of turbofan engines

The effect of nozzle exit geometry on the aerodynamic performance of bypass flow of turbofan engines

Bibliographic Details
Main Author:	Sloan, B.
Published:	Queen's University Belfast 2009
Subjects:	629.13
Online Access:	http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.517527

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