Design development program for C-141 A airframe by Lockheed-Georgia Co is summarized with emphasis on fatigue, damage tolerance, and static strength considerations; fatigue design criteria used for C-141A and C-5A are considered in detail; some significant differences in criteria requirements between C-141A and C-5A are identified together with expected impact on structural design.
Large cargo airplane structural considerations
SAE -- Paper
SAE Meeting ; 1966 Design
1966
7 pages
Conference paper
English
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Large Cargo Airplane Structural Considerations
SAE Technical Papers | 1966
|Design considerations of cargo airplane
Engineering Index Backfile | 1944
|Design considerations of cargo airplane
Engineering Index Backfile | 1943
|Design considerations of cargo airplane
Engineering Index Backfile | 1943
|DESIGN CONSIDERATIONS of the CARGO AIRPLANE
SAE Technical Papers | 1944
|