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Hamid Reza Karbasian

Researcher at Pusan National University

Publications -  26
Citations -  351

Hamid Reza Karbasian is an academic researcher from Pusan National University. The author has contributed to research in topics: Airfoil & Angle of attack. The author has an hindex of 9, co-authored 21 publications receiving 241 citations. Previous affiliations of Hamid Reza Karbasian include Ferdowsi University of Mashhad.

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Simulation of power extraction from tidal currents by flapping foil hydrokinetic turbines in tandem formation

TL;DR: In this article, a code is developed to predict power extraction capacity for the various number of flapping hydrofoils based on the kinematic and hydrodynamic models, which can be used as one of the initial tools to predict the power capacity for obtaining vast concept regarding tidal sites with the flapping foil hydrokinetic turbines.
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Numerical investigations on flow structure and behavior of vortices in the dynamic stall of an oscillating pitching hydrofoil

TL;DR: In this article, the authors numerically investigated the behavior of vortices and flow structure in a dynamic stall phenomenon, especially in post-stall where the flow is highly nonlinear.
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The power extraction by flapping foil hydrokinetic turbine in swing arm mode

TL;DR: In this paper, the power extraction capability by flapping foil hydrokinetic turbine is investigated and the heaving motion of the foil is considered in two different motion patterns including the simple linear translational motion and the rotation of swing arm on which the foil was mounted.
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Fluid structures of flapping airfoil with elliptical motion trajectory

TL;DR: In this paper, the effect of elliptical motion trajectory on the aerodynamic characteristics and propulsive performance of a flapping airfoil is evaluated, where a periodic horizontal motion (forward/backward) is combined with vertical motion (upward/downward) of the airframe to introduce a new kinematic parameter.
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Effect of acceleration on dynamic stall of airfoil in unsteady operating conditions

TL;DR: In this article, the effect of accelerated flow over a moving airfoil is considered and based on the flow field around the air foil the dynamic stall is evaluated, and it is shown that the accelerated flow can significantly influence on the aerodynamic loads and dynamic stall trend.