| People | Locations | Statistics |
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| Naji, M. |
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| Motta, Antonella |
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| Aletan, Dirar |
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| Mohamed, Tarek |
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| Ertürk, Emre |
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| Taccardi, Nicola |
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| Kononenko, Denys |
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| Petrov, R. H. | Madrid |
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| Alshaaer, Mazen | Brussels |
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| Bih, L. |
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| Casati, R. |
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| Muller, Hermance |
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| Kočí, Jan | Prague |
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| Šuljagić, Marija |
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| Kalteremidou, Kalliopi-Artemi | Brussels |
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| Azam, Siraj |
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| Ospanova, Alyiya |
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| Blanpain, Bart |
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| Ali, M. A. |
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| Popa, V. |
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| Rančić, M. |
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| Ollier, Nadège |
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| Azevedo, Nuno Monteiro |
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| Landes, Michael |
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| Rignanese, Gian-Marco |
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Kazancı, Zafer
Queen's University Belfast
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (16/16 displayed)
- 2024Investigation of delamination characteristics in 3D-printed hybrid curved composite beamscitations
- 2024Development of a new progressive damage model for woven fabric compositescitations
- 2024Development of a new progressive damage model for woven fabric compositescitations
- 2024Finite fracture mechanics fracture criterion for free edge delamination
- 2023A three-dimensional Finite Fracture Mechanics model for predicting free edge delamination
- 2023Compressive characterisation of 3D printed composite materials using continuous fibre fabricationcitations
- 2023Three-dimensional semi-analytical investigation of interlaminar stresses in composite laminates
- 2023Tension and compression properties of 3D-printed composites: print orientation and strain rate effectscitations
- 2023A semi-analytical method for measuring the strain energy release rates of elliptical cracks
- 2023Predicting filling efficiency of composite resin injection repaircitations
- 2023Delamination strength comparison of additively manufactured composite curved beams using continuous fiberscitations
- 2023Investigation of several impact angles for predicting bird-strike damage in a riveted eVTOL composite wing
- 2022Comparison of different quasi-static loading conditions of additively manufactured composite hexagonal and auxetic cellular structurescitations
- 2020Crushing Investigation of Crash Boxes Filled with Honeycomb and Re-entrant (auxetic) Latticescitations
- 2012The Nonlinear Dynamic Behaviour of Tapered Laminated Plates Subjected to Blast Loadingcitations
- 2012Friction and wear behaviors of aircraft brake linings materialcitations
Places of action
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document
The Nonlinear Dynamic Behaviour of Tapered Laminated Plates Subjected to Blast Loading
Abstract
In this study, the geometrically nonlinear dynamic behaviour of simply supported tapered laminated composite plates subjected to the air blast loading is investigated numerically. In-plane stiffness, inertia and the geometric nonlinearity effects are considered in the formulation of the problem. The equations of motion for the tapered laminated plate are derived by the use of the virtual work principle. Approximate solution functions are assumed for the space domain and substituted into the equations of motion. Then, the Galerkin method is used to obtain the nonlinear algebraic differential equations in the time domain. The resulting equations are solved by using the finite difference approximation over the time. The effects of the taper ratio, the stacking sequence and the fiber orientation angle on the dynamic response are investigated. The displacement-time and strain-time histories are obtained on certain points in the tapered direction. The results obtained by using the present method are compared with the ones obtained by using a commercial finite element software ANSYS. The results are found to be in an agreement. The method presented here is able to determine the nonlinear dynamic response of simply supported tapered laminated plates to the air blast loading accurately.