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Iman Dayyani

Researcher at Cranfield University

Publications -  35
Citations -  1067

Iman Dayyani is an academic researcher from Cranfield University. The author has contributed to research in topics: Finite element method & Poisson's ratio. The author has an hindex of 13, co-authored 27 publications receiving 747 citations. Previous affiliations of Iman Dayyani include Coventry University & Swansea University.

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A review on shape memory alloys with applications to morphing aircraft

TL;DR: Shape memory alloys (SMAs) as discussed by the authors are a unique class of metallic materials with the ability to recover their original shape at certain characteristic temperatures (shape memory effect), even under high applied loads and large inelastic deformations, or to undergo large strains without plastic deformation or failure (super-elasticity).
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The mechanics of composite corrugated structures: A review with applications in morphing aircraft

TL;DR: A comprehensive review of the literature on corrugated structures can be found in this article, with applications ranging from traditional engineering structures such as Corrugated steel beams through to morphing aircraft wing structures.
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Fluid/Structure-Interaction Analysis of the Fish-Bone-Active-Camber Morphing Concept

TL;DR: In this article, a coupled, partitioned fluid/structure interaction analysis is introduced for calculation of the deformed equilibrium shape, aerodynamic coefficients, and actuation requirements of the fishbone-active-camber morphing concept.
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An equivalent model for trapezoidal corrugated cores based on homogenization method

TL;DR: In this paper, an analytical equivalent model for the mechanical properties of the trapezoidal corrugated core is presented, where a complete set of analytical formulations are derived based on energy approach for elastic modulus in different directions.
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Numerical and Experimental Investigations on Mechanical Behavior of Composite Corrugated Core

TL;DR: In this paper, the tensile and flexural properties of corrugated laminate panels were studied using numerical and analytical methods and compared with experimental data, and the results reveal that the mechanical behavior of the core in tension is sensitive to the variation of core height.