Prediction of induced rolling moments in slender cruciform canard controlled configurations at moderately high angles of attack

Prediction of induced rolling moments in slender cruciform canard controlled configurations at moderately high angles of attack

Bibliographic Details
Main Author:	Gnanasekaran, V.
Published:	Queen's University Belfast 1981
Subjects:	623.4519 Missile aerodynamic design
Online Access:	http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.380490

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