The major objective of this Meeting was to take a further step towards the collection of experience on the fatigue evaluation and substantiation of new helicopters. The Meeting included surveys of current procedures and service experience, consideration of new concepts associated with the introduction of new technologies such as composite materials, new philosophies relevant to service damage and combat damage, and a review of testing techniques and methodologies for airframes and dynamic components. Finally, presentations were made on a European exercise aimed at the development of standardized fatigue load histories for helicopter rotors. (Author)
Helicopter Fatigue Life Assessment
1981
264 pages
Report
No indication
English
Aircraft , Composite Materials , Helicopters , Fatigue life , Symposia , Life expectancy , Determination , Military aircraft , Airframes , Composite materials , Test methods , Standardization , Validation , Fatigue tests(Mechanics) , Fail safe , Gearboxes , Helicopter rotors , Composite structures , Rotor blades(Rotary wings) , Ammunition damage , Damage assessment , Foreign technology , Service life , NATO furnished , NTISDODXA , NTISFNFR
Helicopter Fatigue Life Assessment : Papers
TIBKAT | 1981
Helicopter transmission fatigue life estimation
AIAA | 1988
|Fatigue life estimates for helicopter loading spectra
Tema Archive | 1990
|Helicopter Dynamic Components Fatigue Safe Life Prediction
British Library Conference Proceedings | 2006
|Fatigue Life Evaluation of Helicopter Rotor Heads
Emerald Group Publishing | 1981