This discussion summarizes the highlights of the C-141A airplane program, emphasizing fatigue, damage tolerance, and static strength considerations philosophically and in considerable detail where design criteria are involved. Dynamic considerations are also included insofar as the structural design of the airplane was affected thereby. Finally, some significant differences in criteria requirements between the C-141A and the C-5A are identified together with their expected impact on structural design.
Large Cargo Airplane Structural Considerations
Sae Technical Papers
National Aeronautic and Space Engineering and Manufacturing Meeting ; 1966
1966-02-01
Conference paper
English
Large cargo airplane structural considerations
Engineering Index Backfile | 1966
|Design considerations of cargo airplane
Engineering Index Backfile | 1943
|Design considerations of cargo airplane
Engineering Index Backfile | 1944
|DESIGN CONSIDERATIONS of the CARGO AIRPLANE
SAE Technical Papers | 1944
|STRUCTURAL MATERIALS FOR THE CARGO AIRPLANE
SAE Technical Papers | 1942
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