Projectile aerodynamics : measurement and computation
An experimental study has been performed at M∞=8.2 and Re∞/cm=93000 to examine: 1. The effect of strakes on the aerodynamic characteristics and performance on slender elliptic cone missile configurations. Some information regarding the shock layer was obtained from schlieren pictures. Detailed flow...
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Cranfield University
1997
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| Online Access: | http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.484664 |