1. Military Standard, “Aircraft Structural Integrity Program, Airplane Requirements,” MIL-STD-1530A (USAF), December 1975.
2. Military Specification, “General Specification for Aircraft Structures,” MIL-A-87221, February 1985.
3. Gallagher, J.P., Giessler, F.J., and Berens, A.P., “USAF Damage Tolerant Design Handbook: Guidelines for the Analysis and Design of Damage Tolerant Structures,” Air Force Wright Aeronautical Laboratories, AFWAL-TR-82-3073, May 1984.
4. Military Specification, “Airplane Strength, Rigidity, and Reliability Requirements, Repeated Loads, and Fatigue,” MIL-A-8866B, August 1975.
5. Manning S.D. and Yang, J.N., “USAF Durability Design Handbook: Guidelines for the Analysis and Design of Durable Aircraft Structures,” Air Force Wright Aeronautical Laboratories, AFWAL-TR-83-3027, January 1984.