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2. History of Strength of Materials;Timoshenko,1953
3. Optimum design of joints: the stress severity factor concept;Jarfall;Aeronaut Res Instit Sweden,1967
4. Abelkis, P.R., “Fatigue Strength Design and Analysis for Aircraft Structures, Part 1, Scatter Factors and Design Charts,” AFFDL-TR-66-197, Air Force Flight Dynamics Laboratory, WP-AFB, OH, June, 1967.
5. Babish, C.A., “Testing and Evaluation Requirements for Utilization of an Equivalent Initial Damage Size Method to Establish the Beneficial Effects of Cold Expanded Holes for Development of the Damage Tolerance Initial Inspection Interval,” EZ-SB-17-001, USAF Life Cycle Management Center (LCMC), April, 2017.