United States Army CH-47A Chinook developed by Boeing is twinturbine powered, tandem rotor helicopter designed to provide battlefield mobility for troops, weapons, and equipment; approach employed to solve several structural problems; development of fatigue analysis technique to insure safe life of its critical components; technique includes mission profile, component fatigue strengths, use of top-of-scatter flight loads data, use of Miner's Rule of Cumulative Damage, and evaluation of possible anomalies on fatigue strengths and flight loads.
Some structural considerations in design of Chinook helicopter
SAE -- Paper
SAE Meeting ; 1966 Military
1966
8 pages
Conference paper
English
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Some Structural Considerations in the Design of the Chinook Helicopter
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