Interference fasteners for fatigue-life improvement
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OpenAlex topics: Mechanical Failure Analysis and Simulation · Material Properties and Applications
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References (7)
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1. Fisher, W. A. P., and Winkworth, W. J., “Improvements of the Fatigue Strength of Joints by the Use of Interference Fits,” RAE Structure Rpt. 127 (May 1952).
2. Schijve, J., Broek, D., and Jacobs, F. A., “Fatigue Tests on Aluminum Alloy Lugs with Special Reference to Fretting,” NAA Rsch. Inst. Rpt. No. TNM 2103, Amsterdam, March 1962.
3. Smith, C. R., “Design Applications for Improving Fatigue Resistance of Airplane Structures.”Proc. ASTM,60,581–501 (1960).
4. Smith, C. R., “Tapered Bolts—Their Influence on Fatigue of Airplane Structures,” Convair Rpt. No. ZR-659-053 (May 1960).
5. Smith, C. R., “Linear Strain Theory and Smith Method for Predicting Fatigue Life of Structures for Spectrum Type Loading,” Aerospace Rsch. Labs. Rpt. No. ARL-64-55, Off. Aerospace Rsch., USAF (April 1964).10.21236/AD0600879 ↗
6. “Development of a Method for Assessing the Effects of Cumulative Fatigue Damage of Metallic Structures (U.S. Navy Contract N156-41307),” Naval Air Engrg. Ctr., Philadelphia 12, Pa.
7. Mil. Spec. MIL-A-8866, “Airplane Strength and Rigidity Reliability Requirements, Repeated Loads and Fatigue,” Pg. 4, Spectrum A.