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Large Cargo Airplane Structural Considerations
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1966 by SAE International in United States
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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.
CitationShuler, W., "Large Cargo Airplane Structural Considerations," SAE Technical Paper 660669, 1966, https://doi.org/10.4271/660669.
- Houbolt John C., Steiner Roy, and Pratt Kermit G., “Dynamic Response of Airplanes to Atmospheric Turbulence Including Flight Data on Input and Response, ” JRR-199, NASA, June 1964.
- Byrnes A. L., HensleightW. E., and Tolve L. A., “Effect of Horizontal Stabilizer Vertical Location on the Design of Large Transport Aircraft.”