Rolling tail design and behavior as affected by actuator hinge moment limits
Aircraft Systems and Technology Conference ; 1978 ; Los Angeles , CA , U.S.A.
1978-01-01
Conference paper
Electronic Resource
English
Direct Measurement of Tail Control Panel Hinge Moment Coefficient
Online Contents | 1997
|Vertical tail hinge moment load shedding method for high-speed variable vertical tail aircraft
European Patent Office | 2024
|