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Saeed Karimian Aliabadi
Saeed Karimian Aliabadi
Modares university, Mechanical Engineering Faculty
Verified email at modares.ac.ir - Homepage
Title
Cited by
Cited by
Year
Evaluation of flapping wing propulsion based on a new experimentally validated aeroelastic model
SH Pourtakdoust, SK Aliabadi
Scientia Iranica 19 (3), 472-482, 2012
362012
Effect of platform disturbance on the performance of offshore wind turbine under pitch control
S Karimian Aliabadi, S Rasekh
Wind Energy 23 (5), 1210-1230, 2020
162020
Electricity and hydrogen co-production via scramjet multi-expansion open cooling cycle coupled with a PEM electrolyzer
P Seyedmatin, S Karimian, H Rostamzadeh, M Amidpour
Energy 199, 117364, 2020
152020
Bond graph modeling of a typical flapping wing micro-air-vehicle with the elastic articulated wings
S Karimian, Z Jahanbin
Meccanica 55, 1263-1294, 2020
142020
Parametric study for kinematic optimization of flapping wing vehicle using a new aeroelastic model.
S Karimian Aliabadi, A Ebrahimi
Modares Mechanical Engineering 14 (9), 2014
112014
Modeling and parametric study of a flexible flapping-wing MAV using the bond graph approach
Z Jahanbin, S Karimian
Journal of the Brazilian Society of Mechanical Sciences and Engineering 40, 1-19, 2018
102018
Sensitivity analysis and optimization of delta wing design parameters using CFD-based response surface method
M Aelaei, S Karimian, F Ommi
Journal of applied fluid mechanics 12 (6), 1885-1903, 2019
92019
Aerodynamic modeling of a flexible flapping-wing micro-air vehicle in the bond graph environment with the aim of assessing the lateral control power
S Karimian, Z Jahanbin
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2019
92019
Power and noise performance assessment of a variable pitch vertical axis darrieus type wind turbine
S Karimian, S Rasekh
Journal of the Brazilian Society of Mechanical Sciences and Engineering 43 …, 2021
72021
Accuracy of dynamic stall response for wind turbine airfoils based on semi-empirical and numerical methods
S Rasekh, M Hosseini Doust, S Karimian
Journal of Applied Fluid Mechanics 11 (5), 1287-1296, 2018
72018
Effect of sudden change in free stream velocity on the wind turbine airfoil performance based on boundary element method
SK Aliabadi, S Rasekh
Engineering Analysis with Boundary Elements 101, 360-370, 2019
62019
Toward improving the performance of a variable pitch vertical axis wind turbine (VP-VAWT), Part 2: Multi-objective optimization using NSGA-II with CFD in the loop
S Rasekh, SK Aliabadi
Ocean Engineering 278, 114308, 2023
42023
Periodic Solution for Vibration of Euler-Bernoulli Beams Subjected to Axial Load Using DTM and HA
S Karimian, M Azimi
Scientific Bulletin, Series D 76 (2), 69-76, 2014
42014
Flow modeling in a porous cylinder with regressing walls using semi analytical approach
M Azimi, AM Hedesh, S Karimian
International Journal of Fundamental and Applied Sciences (IJFAS) 3 (3), 42-46, 2014
42014
Toward improving the performance of a variable pitch vertical axis wind turbine (VP-VAWT), Part 1: Sensitivity analysis using Taguchi-CFD approach
S Rasekh, SK Aliabadi, MOL Hansen
Ocean Engineering 279, 114478, 2023
32023
Study the effect of suction flow control on the aerodynamic performance of a wind turbine using 2D section numerical Results
M Asghari, S Karimian Aliabadi, MY Hashemi
Sharif Journal of Mechanical Engineering 37 (1), 79-89, 2021
32021
Effect of solidity on aeroacoustic performance of a vertical axis wind turbine using improved delayed detached eddy simulation
S Rasekh, S Karimian
International Journal of Aeroacoustics 20 (3-4), 390-413, 2021
22021
Comparison of dynamic stall models using numerical and semi-empirical approaches for a wind-turbine airfoil
S RASEKH, AS KARIMIAN, M HOSSEINIDOUST
MODARES MECHANICAL ENGINEERING 18 (3), 282-290, 2018
22018
Flow modeling in a porous cylinder with regressing walls using semi analytical approach
M Azimi, A Hedesh, S Karimian
The International Journal of Multiphysics 9 (1), 75-82, 2015
22015
Experimental study of flapping-wing aerodynamic coefficients and landing performance estimation
SK Aliabadi, MR Parsa, MM Moghadam
Meccanica 58 (4), 711-726, 2023
12023
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