Control effectiveness and hinge-moment measurements at a Mach number of 1.9 of a nose flap and trailing-edge flap on a highly tapered low- aspect-ratio wing
1949-01-10
Miscellaneous
No indication
English
European Patent Office | 2025
|Aerodynamic Hinge Moments on a Sealed-Plain Trailing-Edge Flap at High Mach Number
British Library Conference Proceedings | 1991
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