This document presents symmetric flutter analyses conducted on the all-movable horizontal tail of the Boeing-designed SST. Interaction effects on flutter speed that are produced by the wing, fuselage, control systems and elevator gear ratio are included. Failure conditions of the horizontal-tail actuators are covered. (Author)
Flutter Analysis of an All-Movable Horizontal Tail with Geared Elevator on a Supersonic Transport
1974
60 pages
Report
No indication
English
Aircraft , Aerodynamics , Avionics , Horizontal stabilizers , Flutter , Supersonic transports , Tails(Aircraft) , Hazards , Aeroelasticity , Aviation safety , Aerodynamic loading , Aerodynamic stability , Hydraulic actuators , Failure(Mechanics) , Velocity , Stiffness , Weight , Elevating gear , Equations of Motion , Frequency , SST technology follow on program
AIAA | 1976
|Tema Archive | 1976
|Flutter and LCO of an All-movable Horizontal Tail with Freeplay
British Library Conference Proceedings | 2012
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