Investigation of stress distribution and damage behavior caused by forced installation of a composite bolted joint with a hole-location error

Liang B, Boisse P. A review of numerical analyses and experimental characterization methods for forming of textile reinforcements. Chin J Aeronaut 2021;34(8):143–63.

Gorjipoor A, Van Hoa S, Ganesan R. Numerical model for investigation of the strain distribution in thick composite plates subjected to bolt loads. Aerosp Sci Technol 2016;59:94–102.

Cao ZZ, Zhang F, Zhang DG, et al. Failure mechanisms of bolted flanges in aero-engine casings subjected to impact loading. Chin J Aeronaut 2021;34(12):125–44.

Cao ZQ, Zuo YJ. Electromagnetic riveting technique and its applications. Chin J Aeronaut 2020;33(1):5–15.

Zheng YP, Zhang CY, Tie Y, et al. Tensile properties analysis of CFRP-titanium plate multi-bolt hybrid joints. Chin J Aeronaut 2022;35(3):464–74.

Wang ZH, Li DS, Shen LH, et al. Collaborative force and shape control for large composite fuselage panels assembly. Chin J Aeronaut 2023;36(7):213–25.

Geier N, Davim JP, Szalay T. Advanced cutting tools and technologies for drilling carbon fibre reinforced polymer (CFRP) composites: a review. Compos A 2019;125:105552.

Lecomte J, Bois C, Wargnier H, et al. An analytical model for the prediction of load distribution in multi-bolt composite joints including hole-location errors. Compos Struct 2014;117:354–61.

Yoon D, Kim S, Kim J, et al. Study on bearing strength and failure mode of a carbon-epoxy composite laminate for designing bolted joint structures. Compos Struct 2020;239:112023.

Zuo YJ, Yue T, Jiang RS, et al. Bolt insertion damage and mechanical behaviors investigation of CFRP/CFRP interference fit bolted joints. Chin J Aeronaut 2022;35(9):354–65.

Lekhnitskii SG. Anisotropic plates. New York: Gordon and Breach; 1968.

Persson A. On the stress distribution of cylindrical elastic bodies in contact. Goteborg: Allan Press; 1964.

Ciavarella M, Decuzzi P. The state of stress induced by the plane frictionless cylindrical contact. Ⅰ. The case of elastic similarity. Int J Solids Struct 2001;38(26–27):4507–23.

Ciavarella M, Decuzzi P. The state of stress induced by the plane frictionless cylindrical contact. Ⅰ. The case of elastic similarity. Int J Solids Struct 2001;38(26–27):4525–33.

Liu FR, Lu XH, Zhao LB, et al. An interpretation of the load distributions in highly torqued single-lap composite bolted joints with bolt-hole clearances. Compos B 2018;138:194–205.

Grüber B, Hufenbach W, Kroll L, et al. Stress concentration analysis of fibre-reinforced multilayered composites with pin-loaded holes. Compos Sci Technol 2007;67(7–8):1439–50.

Muskhelishvili N. Some basic problems of the mathematical theory of elasticity: Fundamental equations, plane theory of elasticity, torsion, and bending. Noordhoff Groningen 1963:123–9.

Zhang KD, Ueng CES. Stresses around a pin-loaded hole in orthotropic plates with arbitrary loading direction. Compos Struct 1985;3(2):119–43.

Aluko O, Whitworth HA. Analysis of stress distribution around pin loaded holes in orthotropic plates. Compos Struct 2008;86(4):308–13.

Wu T, Zhang KF, Cheng H, et al. Analytical modeling for stress distribution around interference fit holes on pinned composite plates under tensile load. Compos B 2016;100:176–85.

Song DL, Li Y, Zhang KF, et al. Stress distribution modeling for interference-fit area of each individual layer around composite laminates joint. Compos B 2015;78:469–79.

Hu JS, Zhang KF, Cheng H, et al. Stress analysis and damage evolution in individual plies of notched composite laminates subjected to in-plane loads. Chin J Aeronaut 2017;30(1):447–60.

Kumari S, Pardeep BD. Stress analysis of an infinite plate with single hole by using Airy’s stress function. Mater Today 2022;62:3289–94.

Krishnadasan CK, Shanmugam NS, Sivasubramonian B, et al. Analytical studies and numerical predictions of stresses in shear joints of layered composite panels for aerospace applications. Compos Struct 2021;255:112927.

Liang H, Wang YQ, Tong MB, et al. Multi-scale strength analysis of bolted connections used in integral thermal protection system. Chin J Aeronaut 2018;31(8):1728–40.

Nguyen-Hoang M, Becker W. Stress analysis of finite dimensions bolted joints using the Airy stress function. Int J Solids Struct 2021;224:111023.

Nguyen-Hoang M, Becker W. Stress analysis of a bolted finite dimensions plate under bearing-bypass load interaction using the Airy stress function. Eng Struct 2022;256:113943.

Nguyen-Hoang M, Becker W. Tension failure analysis for bolted joints using a closed-form stress solution. Compos Struct 2020;238:111931.

Nguyen-Hoang M, Becker W. Stress analysis of finite orthotropic plates loaded by a bolted joint. Compos Struct 2021;276:114454.

Zhang B, Xu W, Wu XR. Weight function method and stress intensity factor for two unsymmetric through-thickness and quarter-elliptical corner cracks at circular hole. Eng Fract Mech 2022;264:108361.

Zhai YN, Li XQ, Wang L, et al. Three-dimensional layer-by-layer stress analysis of single-lap, countersunk composite joints with varying joining interface conditions. Compos Struct 2018;202:1021–31.

Cabrera-González JA, Vargas-Silva G, Barroso A. Riveted joints in composites, a practical tool to estimate stresses around the rivet hole. Compos Struct 2021;263:113735.

Hu JS, Zhang KF, Cheng H, et al. Modeling on mechanical behavior and damage evolution of single-lap bolted composite interference-fit joints under thermal effects. Chin J Aeronaut 2021;34(8):230–44.

Khashaba UA, Sebaey TA, Selmy AI. Experimental verification of a progressive damage model for composite pinned-joints with different clearances. Int J Mech Sci 2019;152:481–91.

Cheng H, Luo B, Liang B, et al. Key issues and development trends ofmechanical connection relating to aviation CFRP structure performance. J Adv Manu Sci Tech 2022;2:2022016.

Prakash RV, Hithendra K. Combined influence of pin-hole interference and additional hole on the stress intensity factor for a pin loaded finite plate. Procedia Struct Integr 2020;28:1125–33.

Jiang LX, Dong DW, Xiao S, et al. Experiment and simulation study on bonded, bolted and hybrid bolted/bonded joints of textile CFRP using bimodulus constitutive model. Int J Adhes Adhes 2022;116:103154.

Sajid Z, Karuppanan S, Sallih N, et al. Role of washer size in mitigating adverse effects of bolt-hole clearance in a single-lap, single-bolt basalt composite joint. Compos Struct 2021;266:113802.

Liu EX, Liu YM, Chen YL, et al. Measurement method of bolt hole assembly stress based on the combination of ultrasonic longitudinal and transverse waves. Appl Acoust 2022;189:108603.

Kou JF, Xu F, Zhang XY, et al. Analytical solution of shear stiffness for double-lap bolted joints with clearances. Acta Mater Compos Sin 2018;35(6):1510–7 [Chinese].

Kou JF, Xu F. Three-dimensional bearing stress distribution at bolt-hole in quasi-isotropic laminates. Acta Mater Compos Sin 2018;35(12):3360–7 [Chinese].

Richard RM, Blacklock JR. Finite element analysis of inelastic structures. AIAA J 1969;7(3):432–8.

Huang CH, Lee YJ. Experiments and simulation of the static contact crush of composite laminated plates. Compos Struct 2003;61(3):265–70.

Chang KY, Llu S, Chang FK. Damage tolerance of laminated composites containing an open hole and subjected to tensile loadings. J Compos Mater 1991;25(3):274–301.

Linde P, Pleitner J, de Boer H, et al. Modelling and simulation of fibre metal laminates. ABAQUS Users’ Conf. 2004.

Zhao LB, Li Y, Zhang JY, et al. A novel material degradation model for unidirectional CFRP composites. Compos B 2018;135:84–94.

Hu JS, Zhang KF, Yang QD, et al. An experimental study on mechanical response of single-lap bolted CFRP composite interference-fit joints. Compos Struct 2018;196:76–88.