Comparison of fatigue life and flexibility between aluminum-composite and aluminum–aluminum bolted joints
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Research context
OpenAlex topics: Fatigue and fracture mechanics · Structural Load-Bearing Analysis · Mechanical Behavior of Composites
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References (24)
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1. Fatigue of structures and materials in the 20th century and the state of the art10.1016/S0142-1123(03)00051-3 ↗
2. Optimum design of joints: the stress severity factor concept
3. Fatigue life predictions for riveted lap joints10.1016/j.ijfatigue.2016.09.007 ↗
4. Kapidžić Z. Development of data and method for fatigue sizing of bolted joints in AA7050-T7451 and AA2050-T84. In: A Review of aeronautical fatigue investigations in Sweden during the period April 2017 to March 2019, 36th ICAF Conference, 2019.
5. Prediction of fretting fatigue crack initiation in double lap bolted joint using continuum damage mechanics10.1016/j.ijfatigue.2014.11.012 ↗
6. Continuum damage mechanics based approach to study the effects of the scarf angle, surface friction and clamping force over the fatigue life of scarf bolted joints10.1016/j.ijfatigue.2017.04.008 ↗
7. A simplified continuum damage mechanics based modeling strategy for cumulative fatigue damage assessment of metallic bolted joints10.1016/j.ijfatigue.2019.105302 ↗
8. Ultrasonic detection of fretting fatigue damage at bolt joints of aluminum alloy plates10.1016/j.ijfatigue.2009.03.017 ↗
9. Schijve · 2008
10. Revealing the competitive fatigue failure behaviour of CFRP-aluminum two-bolt, double-lap joints10.1016/j.compstruct.2020.112166 ↗
11. Mechanical joining of fibre reinforced polymer composites to metals—A review. Part I: Bolted joining10.3390/polym12102252 ↗
12. Shivakumar K, Crews J. Bolt Clampup relaxation in a graphite/epoxy laminate. In: O’Brien T, editor. Long-term behavior of composites. West Conshohocken, PA.
13. Coefficient of friction for aluminum in contact with a carbon fiber epoxy composite10.1016/j.triboint.2003.11.008 ↗
14. Local fatigue behaviour of CFRP bolted joints10.1016/S0266-3538(01)00200-7 ↗
15. EN 4495:2006 Aerospace series - Bolts, normal hexagonal head, close tolerance normal shank, short thread, in titanium alloy, anodized, with aluminium pigmented coating, metric series - Classification: 1100 MPa (at ambient temperature) / 315 °C. Standard, European Commitee for Standardization, Brussels, June 2006.
16. Ansell H. Structural integrity assessment of Gripen NG aircraft, In: Proceedings of the 34th conference and the 28th symposium of the international committee on aeronautical fatigue and structural integrity.
17. Rouchon J. Fatigue and damage tolerance evaluation of structures: The composite material response, In: 22th Plantema memorial lecture, 25th ICAF symposium, 2009.
18. ASTM D5961/D5961M-17. Standard test method for bearing response of polymer–matrix composite laminates. Vol. 15.03. Composite materials.
19. Huth H. Influence of fastener flexibility on the prediction of load transfer and fatigue life for multiple-row joints. In: Potter JM, editor. Fatigue in mechanically fastened composite and metallic joints, ASTM STP 927.
20. 2016
21. Barbero · 2013
22. Pilkey · 2008
23. 1990
24. An analytical joint stiffness model for load transfer analysis in highly torqued multi-bolt composite joints with clearances10.1016/j.compstruct.2015.06.003 ↗