Aircraft Load Alleviation and Mode Stabilization (LAMS) Flight Demonstration Test Analysis
1969
176 pages
Report
No indication
English
Aircraft , Jet bombers , Flight control systems , Jet transport planes , Gust loads , Stabilization , Aerodynamic control surfaces , Airframes , Fatigue(Mechanics) , Damage , Flight testing , Handling , B-52e aircraft , B-52 aircraft , C-5 aircraft , C-5a aircraft , Fly by wire flight control systems , Lams(Load alleviation and mode stabilization) , Load alleviation and mode stabilization