Stiffness behavior of hybrid laminated composites with surface crack

• Autorzy: Güneş A. , Şahin Ö. A.

Identyfikatory

DOI

10.5604/18972764.1229632

• Języki publikacji: EN

Abstrakty

EN

Purpose: The purpose of this paper investigates to stiffness behavior of hybrid laminated composites with surface crack. Design/methodology/approach: Hybrid laminated composites has 18 layers and 90x25 mm size with two different layers line up. The low velocity impact test of hybrid laminated composites carried on 3 m/sec with a/t=0.4 and a/c=0.4 surface crack parameters. Findings: The results are presented as the change of force-time and force-displacement graphs. As a result of this study, effects of stacking sequence on hybrid composite plates were analysed. Research limitations/implications: The research of stiffness behavior or dynamic response of hybrid laminated composites can contribute to developing new composite materials. Practical implications: These hybrid laminated composites materials could be used for different aviation areas. Originality/value: This paper is based on studies from Selçuk University and all the experiments and results were conducted by me.

Słowa kluczowe

EN

low velocity impact; surface crack; laminated composite

PL

udar o małej prędkości; pęknięcie powierzchniowe; kompozyt warstwowy

• Wydawca: International OCSCO World Press
• Czasopismo: Archives of Materials Science and Engineering
• Rocznik: 2016
• Tom: Vol. 80, nr 2
• Strony: 49--52
• Opis fizyczny: Bibliogr. 11 poz.

Twórcy

autor

Güneş A.

• Department of Mechanical Engineering, Selcuk University, Konya, Turkey

autor

Şahin Ö. A.

• Department of Mechanical Engineering, Selcuk University, Konya, Turkey

Bibliografia

• [1] K.F. Nilsson, L.E. Asp, J.E. Alpman, L. Nystedt, Delamination buckling and growth for delaminations at different depths in a slender composite panel, International Journal of Solids and Structures 38 (2001) 3039-3071.
• [2] C. Oh, J. Song, Crack growth and closure behaviour of surface cracks under pure bending loading, International Journal of Fatigue 23 (2001) 251-258.
• [3] A. Gunes, Investigation of dynamic behaviours of hybrid stacked composite laminates with surface crack, Ms Thesis, Selçuk University, Department of Mechanical Engineering, 2013.
• [4] G. Belingardi, R. Vadori, Low velocity impact tests of laminate glass-fiber-epoxy matrix composite material plates, International Journal of Impact Engineering 27 (2002) 213-229.
• [5] F. Aymerich, P. Priolo, Characterization of fracture modes in stitched and unstitched cross-ply laminates subjected to low-velocity impact and compression after impact loading, International Journal of mpact Engineering 35 (2008) 591-608.
• [6] T.L. Anderson, Fracture mechanics: Fundamentals and applications, CRC Press, 1995.
• [7] Y. Tang, L. Ye, Z. Zhang, K. Friedrich, Interlaminar fracture toughness and CAI strength of fibrereinforced composites with nanoparticles-A review, Composite Science and Technology 86 (2013) 26-37.
• [8] M.A. Hassan, S. Naderi, A.R. Bushroa, Low velocity impact damage of woven fabric composites: Finite element simulation and experimental verification, Materials and Design 53 (2014) 706-718.
• [9] M.D. Kulkardi, R. Goel, N.K. Naik, Effect of back pressure on impact and compression-after-impact characteristics of composites, Composite Structures 93 (2011) 944-951.
• [10] W. Trabelsi, L. Michel, R. Othomene, Effects of stitching on delamination of satin weave carbon-epoxy laminates under mode I, mode II and mixed-mode I/II loadings, Applied Composite Materials 17 (2010) 575- 595.
• [11] D.D.L. Chung, Structural composite materials tailored for damping, Journal of Alloys and Compounds 355 (2003) 216-223.

Uwagi

PL

Opracowanie ze środków MNiSW w ramach umowy 812/P-DUN/2016 na działalność upowszechniającą naukę (zadania 2017).