The aeroelastic response of a two-dimensional airfoil with bilinear and cubic structural nonlinearities SJ Price, H Alighanbari, BHK Lee Journal of fluids and structures 9 (2), 175-193, 1995 | 256 | 1995 |
Poststability behavior of a two-dimensional airfoil with a structural nonlinearity SJ Price, BHK Lee, H Alighanbari Journal of Aircraft 31 (6), 1395-1401, 1994 | 149 | 1994 |
An investigation into the effects of unsteady parameters on the aerodynamics of a low Reynolds number pitching airfoil MR Amiralaei, H Alighanbari, SM Hashemi Journal of Fluids and Structures 26 (6), 979-993, 2010 | 121 | 2010 |
Particle swarm optimization applied to spacecraft reentry trajectory A Rahimi, K Dev Kumar, H Alighanbari Journal of Guidance, Control, and Dynamics 36 (1), 307-310, 2013 | 107 | 2013 |
The post-Hopf-bifurcation response of an airfoil in incompressible two-dimensional flow H Alighanbari, SJ Price Nonlinear Dynamics 10, 381-400, 1996 | 107 | 1996 |
Fault estimation of satellite reaction wheels using covariance based adaptive unscented Kalman filter A Rahimi, KD Kumar, H Alighanbari Acta astronautica 134, 159-169, 2017 | 98 | 2017 |
A physical explanation of the destabilizing effect of damping C Semler, H Alighanbari, MP Pai¨ doussis | 53 | 1998 |
Flow field characteristics study of a flapping airfoil using computational fluid dynamics MR Amiralaei, H Alighanbari, SM Hashemi Journal of Fluids and Structures 27 (7), 1068-1085, 2011 | 52 | 2011 |
Fault detection and isolation of control moment gyros for satellite attitude control subsystem A Rahimi, KD Kumar, H Alighanbari Mechanical Systems and Signal Processing 135, 106419, 2020 | 47 | 2020 |
Fault isolation of reaction wheels for satellite attitude control A Rahimi, KD Kumar, H Alighanbari IEEE Transactions on Aerospace and Electronic Systems 56 (1), 610-629, 2019 | 35 | 2019 |
Enhanced adaptive unscented Kalman filter for reaction wheels A Rahimi, KD Kumar, H Alighanbari IEEE Transactions on Aerospace and Electronic Systems 51 (2), 1568-1575, 2015 | 30 | 2015 |
Influence of heat transfer on the aerodynamic performance of a plunging and pitching NACA0012 airfoil at low Reynolds numbers DF Hinz, H Alighanbari, C Breitsamter Journal of Fluids and Structures 37, 88-99, 2013 | 24 | 2013 |
Design and analysis of a grid patch multi-stable composite A Algmuni, F Xi, H Alighanbari Composite Structures 246, 112378, 2020 | 22 | 2020 |
Failure prognosis for satellite reaction wheels using Kalman filter and particle filter A Rahimi, KD Kumar, H Alighanbari Journal of Guidance, Control, and Dynamics 43 (3), 585-588, 2020 | 21 | 2020 |
Nonlinear control design of an airfoil with active flutter suppression in the presence of disturbance S Afkhami, H Alighanbari IET Control Theory & Applications 1 (6), 1638-1649, 2007 | 20 | 2007 |
Aeroelastic response of an airfoil-aileron combination with freeplay in aileron hinge H Alighanbari Journal of aircraft 39 (4), 711-713, 2002 | 16 | 2002 |
Controller design for rotary inverted pendulum system using particle swarm optimization algorithm A Rahimi, K Raahemifar, K Kumar, H Alighanbari 2013 26th IEEE Canadian Conference on Electrical and Computer Engineering …, 2013 | 12 | 2013 |
Analysis of nonlinear aeroelastic signals H Alighanbari, BHK Lee Journal of aircraft 40 (3), 552-558, 2003 | 10 | 2003 |
Numerical modelling of a low Reynolds number plunging airfoil flow field characteristics MR Amiralaei, H Alighanbari, SM Hashemi Journal of Aerospace Engineering, Proceedings of the Institution of …, 2013 | 7 | 2013 |
An inclined FGM beam under a moving mass considering Coriolis and centrifugal accelerations V Shokouhifard, S Mohebpour, P Malekzadeh, H Alighanbari Steel and Composite Structures, An International Journal 35 (1), 61-76, 2020 | 6 | 2020 |