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Material Selection Procedures for Advanced Transport Aircraft
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English
Abstract
This paper will discuss the procedures used for material selection that were developed and used for two Advanced Metallic Structures, Advanced Development Programs (AMS/ADP) sponsored by the Air Force Flight Dynamics Laboratory (AFFDL) under joint management and direction of AFFDL and the Air Force Materials Laboratory, Wright-Patterson Air Force Base, Ohio. The relationship of structural properties and the role of fracture mechanics in material selection are covered. The application of the selection criteria is demonstrated as it was applied to the Advanced Metallic Air Vehicle Structure.
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Authors
Citation
Shults, J., "Material Selection Procedures for Advanced Transport Aircraft," SAE Technical Paper 730884, 1973, https://doi.org/10.4271/730884.Also In
References
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- “Advanced Metallic Air Vehicle Structure Program.” Phase Ib Preliminary Design Summary Technical Report March 1973
- “Advanced Metallic Air Vehicle Structures Program.” Second Six Month Phase Ib and II Technical Report June 1973
- “Advanced Metallic Structure: Air Superiority Fighter Wing Design for Improved Cost, Weight, and Integrity.” June 1973
- Butler Joseph P. “The Material Selection and Structural Development Process for Aircraft Structural Integrity Under Fatigue Considerations.” Proceedings of the Air Force Conference on Fatigue and Fracture of Aircraft Structures and Materials December 1969 17 44
- Haupt Ulrich “Interface of Materials and Structure, Part I, Basic Design Considerations.” U.S. Naval Postgraduate School November 1961
- Rolfe S. T. “Fracture Criteria for Structural Steels.” ASM Seminar on Fracture Control Philadelphia 1970
- Irwin G. R. “Relation of Crack-Toughness Measurements to Practical Applications.” Paper 62-MET-15 presented at ASME Metals Engineering Conference Cleveland April 1962
- Wood Howard A. “Fracture Control Procedures for Aircraft Structural Integrity.” Technical Report July 1971