Rolling tail design and behavior as affected by actuator hinge moment limits
Aircraft Systems and Technology Conference ; 1978 ; Los Angeles , CA , U.S.A.
01.01.1978
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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
Europäisches Patentamt | 2024
|