Experimental investigation on the effect of forced assembly on fatigue behavior of single-lap, countersunk composite bolted joints
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OpenAlex topics: Mechanical Behavior of Composites · Fatigue and fracture mechanics · Mechanical stress and fatigue analysis
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References (37)
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1. Airbus A350 XWB update10.1016/S0034-3617(10)70212-5 ↗
2. High performance drilling of T800 CFRP composites by combining ultrasonic vibration and optimized drill structure10.1016/j.ultras.2023.107097 ↗
3. A progressive fatigue damage model for composite structures in hygrothermal environments10.1016/j.ijfatigue.2018.02.019 ↗
4. Z. Wang, D. Li, L. Shen, Y. Sui, Y. Zhai, Collaborative force and shape control for large composite fuselage panels assembly, Chin. J. Aeronaut. 36 (7) 213-225.10.1016/j.cja.2023.02.013 ↗
5. Influence of hole eccentricity on failure progression in a double shear bolted joint (DSBJ)10.1016/j.compscitech.2018.09.011 ↗
6. Role of the surface quality on the mechanical behavior of CFRP bolted composite joints10.1016/j.ijfatigue.2015.06.012 ↗
7. Stress analysis of single-bolt, single-lap, countersunk composite joints with variable bolt-hole clearance10.1016/j.compstruct.2011.10.004 ↗
8. Fatigue characteristics of the bolted joints for unidirectional composite laminates10.1016/j.compstruct.2004.10.013 ↗
9. Effects of joint geometry and bolt torque on the structural performance of single bolt tension joints in pultruded GRP sheet material10.1016/0263-8223(95)00071-2 ↗
10. Effects of geometrical and material features on damage onset and propagation in single-lap bolted composite joints under tensile load: Part I - experimental studies10.1177/0021998305052026 ↗
11. Effects of geometrical and material features on damage onset and propagation in single-lap bolted composite joints under tensile load: Part II - numerical studies10.1177/0021998305052027 ↗
12. Effects of stacking sequence and clamping force on the bearing strengths of mechanically fastened joints in composite laminates10.1016/S0263-8223(01)00005-8 ↗
13. Bolt-hole clearance effects and strength criteria in single-bolt, single-lap, composite bolted joints10.1016/S0266-3538(02)00088-X ↗
14. Thermal-mechanical-equivalent fatigue load method for mechanically fastened Hybrid-material structures10.1016/j.ijfatigue.2023.107906 ↗
15. An experimental investigation into quasi-static and fatigue damage development in bolted-hole specimens10.1016/j.compositesb.2015.03.051 ↗
16. Spectrum fatigue loading of composite bolted joints—small cycle elimination10.1016/j.ijfatigue.2005.01.016 ↗
17. Experimental study on fatigue resistance of composite joints with protruding-head bolts10.1016/S0263-8223(01)00127-1 ↗
18. Fatigue bearing failure of CFRP composite in biaxially loaded bolted joints at elevated temperature10.1016/j.compstruct.2015.03.031 ↗
19. Influence of interference-fit size on bearing fatigue response of single-lap carbon fiber reinforced polymer/Ti alloy bolted joints10.1016/j.triboint.2015.08.044 ↗
20. Effects of bolt torque tightening on the strength and fatigue life of airframe FRP laminate bolted joints10.1016/j.compositesb.2017.05.059 ↗
21. Static and fatigue behavior of pultruded FRP multi-bolted joints with basalt FRP and hybrid steel-FRP bolts10.1016/j.compstruct.2019.03.085 ↗
22. Fatigue behaviour and failure mechanism of the thin/thick-ply hybrid laminated composite bolted joints10.1016/j.compstruct.2022.115636 ↗
23. B. Chouvion, A. Popov, S. Ratchev, C. Mason, M. Summers, Interface management in wing-box assembly, SAE Technical Paper. 2011-01-2640; 2011.10.4271/2011-01-2640 ↗
24. Robotic compliant assembly for complex-shaped composite aircraft frame based on Gaussian process considering uncertainties10.1016/j.cja.2024.03.022 ↗
25. Feasibility analysis of composite fuselage shape control via finite element analysis10.1016/j.jmsy.2018.01.008 ↗
26. Flexible automated assembly systems for large CFRP-structures10.1016/j.protcy.2014.09.004 ↗
27. Active learning for gaussian process considering uncertainties with application to shape control of composite fuselage10.1109/TASE.2020.2990401 ↗
28. J. Goering, R. Bohlmann, S. Wanthal, E. Kautz, L. Neri, Assembly induced delaminations in composite structures, In: Ninth DOD (NASA) FAA Conference on Fibrous. Composites in Structural Design; 1992. p. 1353-1377.
29. H. Kan, E. Kautz, L. Neri, Analysis of composite structures with delaminations under combined bending and compression, In: Ninth DOD (NASA) FAA Conference on Fibrous Composites in Structural Design; 1992. p. 197-224.
30. An experimental study on the effect of joining interface condition on bearing response of single-lap, countersunk composite-aluminum bolted joints10.1016/j.compstruct.2015.08.078 ↗
31. Effect of preload and shim types on the mechanical properties of composite-aluminium bolted joints: Proc10.1177/09544062211007172 ↗
32. An enhanced spring-mass model for stiffness prediction in single-lap composite joints with considering assembly gap and gap shimming10.1016/j.compstruct.2017.12.041 ↗
33. Effect of forced assembly on bearing performance of single-lap, countersunk composite bolted joints–Part Ⅰ: Experimental investigation10.1016/j.compstruct.2023.117201 ↗
34. ASTM D5961. Standard test method for bearing response of polymer matrix composite laminates. Am Soc Testing Mater; 2013.
35. Effect of forced assembly on bearing performance of single-lap, countersunk composite bolted joints–Part II: Numerical investigation10.1016/j.compstruct.2023.117169 ↗
36. ASTM D6873. Standard practice for bearing fatigue response of polymer matrix composite laminates. Am Soc Testing Mater; 2014.
37. ASTM E739. Standard Practice for Statistical Analysis of Linear or Linearized Stress-Life (S-N) and Strain-Life (ε-N) Fatigue Data. Am Soc Testing Mater; 2015.