Transient Dynamic Response of Clamped-Free Hybrid Composite Circular Cylindrical Shells
Source abstract
Abstract
Dynamic response of multilayer circular cylindrical shells composed of hybrid composite materials subjected to lateral impulse load is studied in this paper. The boundary conditions (B.C.s) are considered to be clamped-free. Both isotropic (metal) and orthotropic (composite) layers are used simultaneously in the hybrid lamination. There is no limitation for fibre orientation. First order shear deformation theory (FSDT) and Love’s first approximation theory are utilized in the shell’s equilibrium equations. Equilibrium equations for free and forced vibration problems of the shell are solved using Galerkin method. Finally, time response of displacement components of Fibre-Metal Laminate (FML) cylindrical shells is derived using mode superposition method. The effect of lay up, material properties, fibre orientation and volume fraction of metal layers on the dynamic response of the shell are investigated. New interesting results are obtained and discussed providing a helpful insight for aircraft structure’s designers.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Composite Structure Analysis and Optimization · Vibration and Dynamic Analysis · Structural Analysis and Optimization
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (16)
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1. Jafari, A.A., Khalili, S.M.R., Azarafza, R.: Transient dynamic response of composite circular cylindrical shells under radial impulse load and axial compressive loads. Thin-Walled Struct. 43, 1763–1786 (2005)10.1016/j.tws.2005.06.009 ↗
2. Khalili, S.M.R., Azarafza, R., Davar, A.: Transient dynamic response of initially stressed composite circular cylindrical shells under radial impulse load. Compos. Struct. 89(2), 275–284 (2009)10.1016/j.compstruct.2008.08.002 ↗
3. Lemanski, S.L., Nurick, G.N., Langdon, G.S., Simmons, M.S., Cantwell, W.J., Schleyer, G.K.: Understanding the behaviour of fibre metal laminates subjected to localised blast loading. Compos. Struct. 76, 82–87 (2006)10.1016/j.compstruct.2006.06.012 ↗
4. Karagiozova, D., Langdon, G.S., Nurick, G.N., Kim Yuen, C.: Simulation of the response of fibre-metal laminates to localised blast loading. Int. J. Impact Eng. doi: 10.1016/j.ijimpeng.2009.04.001 (2009)10.1016/j.ijimpeng.2009.04.001 ↗
5. Vogelesang, L.B., Vlot, A.: Development of fibre metal laminates for advanced aerospace structures. J. Mater. Process. Technol. 103, 1–5 (2000)10.1016/S0924-0136(00)00411-8 ↗
6. Sinke, J.: Development of Fibre Metal Laminates: Concurrent multi scale modeling and testing. J. Mater. Sci. 41, 6777–6788 (2006)10.1007/s10853-006-0206-5 ↗
7. Hebsur, M.G., Noebe, R.D., Revilock, D.M.: Impact resistance of lightweight hybrid structures for gas turbine engine fan containment applications. J. Mater. Eng. Perform. 12(4), 470 (2003)10.1361/105994903770343033 ↗
8. Vlot, A., Gunnink, J.W.: Fibre metal laminates — an introduction. Kluwer Academic, Dordrecht / Boston / London (2001)10.1007/978-94-010-0995-9 ↗
9. Cid Alfaro, M.V.: Multiscale analysis of fibre metal laminates. PhD thesis, Delft University of Technology, The Netherlands (2008)
10. Asundi, A., Choi, A.Y.N.: Fiber metal laminates: An advanced material for future aircraft. J. Mater. Process. Technol. 63, 384–394 (1997)10.1016/S0924-0136(96)02652-0 ↗
11. Gong, S.W., Lam, K.Y.: Effects of structural damping and stiffness on impact response of layered structures. AIAA J. 38(9), 1730–1735 (2000)10.2514/2.1161 ↗
12. Malekzadeh, K., Khalili, M.R., Mittal, R.K.: Response of composite sandwich panels with transversely flexible core to low-velocity transverse impact: A new dynamic model. Int. J. Impact Eng. 34, 522–543 (2007)10.1016/j.ijimpeng.2005.10.002 ↗
13. Vinson, J.R.: The mechanical behavior of shells composed of isotropic and composite materials. Kluwer academic, Dordrecht/Boston/London (1993)10.1007/978-94-015-8141-7 ↗
14. Altenbach, H., Altenbach, J., Kissing, W.: Mechanics of composite structural elements, p. 458. Springer-Verlag, Berlin (2004)10.1007/978-3-662-08589-9 ↗
15. Lam, K.Y., Loy, C.T.: Influence of boundary conditions and fiber orientation on the natural frequencies of thin orthotropic laminated cylindrical shells. Compos. Struct. 31, 21–30 (1995)10.1016/0263-8223(94)00054-9 ↗
16. Abaqus, Inc.: Abaqus version 6.7 user’s manual. Pawtucket, RI, USA (2007)