Publications
Papers
in Refereed Journals
1. F. Barzegar, S.
Mohebpour, and H. Alighanbari, “Multi-crack detection in general
cross-section swept wings based on natural frequency changes”, Journal
of Vibration and Control, Vol 27, Issue 21-22, pp. 2616-2629, Nov. 2021.
2. A. Algmuni, F. Xi, and H. Alighanbari, "Flexible
joints for a grid-based multi-stable composite morphing skin”, Composite
Structures, Vol 259, March 2021.
3. A.
Algmuni, F. Xi, and H. Alighanbari, “Design and analysis of a grid patch
multi-stable composite”, Composite Structures, Vol 246, Aug 2020.
4. M. Melville, G. Bramesfeld, A. Kolaei and H. Alighanbari, “Aeroelastic Tailoring for
Gust Energy Extractions”, Journal of Aerospace Engineering, Vol 33 Issue 4, Aug 2020.
5.
A. Rahimi, K. Kumar, and
H. Alighanbari, “Failure prognosis for satellite reaction wheels using kalman filter and particle filter”, Journal of
Guidance, Control, and Dynamics, Vol 43 Issue 3, pp. 585-588, Mar 2020.
6.
V. Shokouhifard, S.
Mohebpour, P. Malekzadeh and H. Alighanbari, “An inclined FGM beam under
a moving mass considering Coriolis and centrifugal accelerations”, Steel
and Composite Structures, Vol 35, Issue 1, pp.61-76, 2020
7. A. Rahimi, K. Kumar, and H. Alighanbari, “Fault
detection and isolation of control moment gyros for satellite attitude control
subsystem”, Mechanical Systems and Signal Processing, Vol 135, Jan
2020.
8. A. Rahimi, K. Kumar, and H. Alighanbari, "Fault
Isolation of Reaction Wheels for Satellite Attitude Control", IEEE-Transactions
on Aerospace and Electronic Systems, Vol 56 Issue 1, pp. 610-629, Oct 2019.
9. B. Raeisi and H. Alighanbari, “Simulation and analysis
of flow around tilting asymmetric ducted fans mounted at the wing tips of a
vertical take-off and landing unmanned aerial vehicle”, Journal of Aerospace Engineering (Part G:) Vol. 232 Issue 15, pp. 2870-2897, Nov. 2018.
10. B. Raeisi and H. Alighanbari, “Effects of tilting rate variations
on the aerodynamics of the tilting ducted fans mounted at the wing tips of a
vertical take-off and landing unmanned aerial vehicle”, Journal of Aerospace Engineering, (Part G:) Vol. 232 Issue 10, pp. 1803-1813, July 2018.
11. A.
Rahimi, K. Kumar, and H. Alighanbari, “Fault estimation of satellite
reaction wheels using covariance based adaptive unscented Kalman filter”,
Acta Astronautica,
Vol. 134, pp. 159-169, May 2017,
12. A.
Rahimi, K. Kumar, and H. Alighanbari, “Enhanced Adaptive Unscented Kalman
Filter for Reaction Wheels”, IEEE-TAES,
Vol 51, Issue 2, pp. 1568-1575,
2015.
13. B.
Raeisi and H. Alighanbari, “CFD Analysis of Oscillating Blades for Small
Horizontal Axis Wind Turbines in Dynamic Stall condition”, Wind Engineering, Vol. 38, Issue 5, pp. 499-522, Oct. 2014
14. M.R.
Amiralaei, H. Alighanbari and S.M. Hashemi, “Numerical modeling of a low
Reynolds number plunging airfoil flow field characteristics”, Journal of Aerospace Engineering (Proc.
of the Inst. of Mech. Eng., Part G:)Vol. 227 Issue. 8, pp. 1251-1264, Aug.
2013.
15. M.R.
Amiralaei, H. Alighanbari and S.M. Hashemi, “On the force signatures of a
pair of multi-plunging airfoils”, Journal
of Aerospace Engineering (Proc. of the Inst. of Mech. Eng., Part G:), Vol. 227 Issue 4, pp. 647-662, Apr. 2013.
16. D.F. Hinz, H. Alighanbari and C. Breitsamter,
“Influence of heat transfer on the aerodynamic performance of a plunging
and pitching NACA0012 airfoil at low Reynolds numbers”, Journal of Fluids and Structures, Vol 37, pp. 88–99 Feb. 2013.
17. A. Rahimi, K. Kumar, and H. Alighanbari,
“Particle Swarm Optimization Applied to Spacecraft Re-entry
Trajectory”, AIAA Journal of
Guidance, Control, and Dynamics, Vol. 36 Issue 1, pp. 307-311, Jan. 2013.
18. M.R. Amiralaei, H. Alighanbari and S.M.
Hashemi, “Flow field
characteristics study of a flapping airfoil using computational fluid
dynamics”, Journal of Fluids and
Structures, Vol. 27, Issue 7, pp. 1068-1085, October 2011.
19. H. Alighanbari, “Derivation of Ordinary
Differential Equations for a 3-DOF Airfoil-Aileron Combination Subjected to
Unsteady Incompressible Flow”, Journal
of Mathematics in Engineering, Science and Aerospace, Vol 1, No. 2, pp.
149-157, 2010.
20. M.R. Amiralaei, H. Alighanbari and S.M.
Hashemi, “An investigation into the effects of unsteady parameters on the
aerodynamics of a low Reynolds number pitching airfoil”, Journal of Fluids and Structures, Vol.
26, Issue 6, pp. 979-993, August 2010.
21. M.R. Amiralaei, H. Alighanbari and S.M.
Hashemi, “Effects of Reynolds Number and Pitching Amplitude of
Oscillation on Flapping Aerodynamics”, Journal of Mathematics in Engineering, Science and Aerospace, Vol
1, No. 4, pp. 393-405, 2010.
22. H. Alighanbari and S. Hashemi, “Derivation
of ODEs and Bifurcation Analysis of a Two-DOF Airfoil”, International
Journal of Aerospace Engineering, Volume 2009 Article ID 248930, 7 pages, 2009.
23. S.R. Borneman, S. Hashemi, and H. Alighanbari, “Vibration
Analysis of Cracked Stepped Laminated Composite Beams”, International
Journal of Vehicle Structures: Design, Analysis and Optimization, Vol 1, No
1-3, August 2009.
24. S.R.
Borneman, S. Hashemi, and H. Alighanbari, “Preliminary Flutter Analysis
of a Doubly Tapered Composite Wing Using Refined Dynamic Finite
Elements”, International Review of Aerospace Engineering, Vol. 2,
No. 1, pp. 44-51, 2009.
25. S.R.
Borneman, S. Hashemi, and H. Alighanbari, “Vibration Analysis of Doubly
Coupled Cracked Composite Beams: An Exact Dynamic Stiffness Matrix” International
Review of Aerospace Engineering, Vol. 1, No. 3, pp. 298-309, 2008.
26. S.
Hashemi, S.R. Borneman, and H. Alighanbari, “Vibration of Cracked
Composite Beams: a Dynamic Finite Element”, International
Review of Aerospace Engineering, Vol. 1, No.1, pp. 110-121, 2008.
27. S. Afkhami and H. Alighanbari, “Nonlinear control design
of an airfoil with active flutter suppression in the presence of
disturbance”, Control Theory and Aplications,
IET, Vol. 1, Issue 6, pp. 1638-1649, 2007.
28. A. Varvani and H. Alighanbari, “Material Cyclic Behaviour of Panels at Supersonic Speeds”, Journal
of Materials Processing Technology, Vol. 152, No. pp. 84-90, 2004.
29. H.
Alighanbari and B.H.K Lee, "Analysis of Nonlinear Aeroelastic
Response", AIAA Journal of Aircraft, Vol. 40, No. 3, pp.430-437,
May/June 2003.
30. H.
Alighanbari, "Aeroelastic Response of an Airfoil-Aileron Combination with
Freeplay in Aileron Hinge", AIAA Journal of Aircraft, Vol. 39, No.
4, pp.711-713, 2002.
31. C. Semler, H. Alighanbari
and M.P. Paidoussis, “A Physical Explanation of
the Destabilizing Effect of Damping”, Journal
of Applied Mechanics, Vol. 65, pp. 642-648, 1998.
32. H. Alighanbari and S.J. Price, “The Post-Hopf-Bifurcation Response of an Airfoil in Incompressible
Two-Dimensional Flow”, Nonlinear
Dynamics, Vol. 10, pp. 381-400, 1996.
33. S.J. Price, H. Alighanbari and B.H.K. Lee,
“The Aeroelastic Response of a Two-Dimensional Airfoil with Bilinear and
Cubic Structural Nonlinearities
34. S.J. Price, B.H.K. Lee and H. Alighanbari,
“Postinstability Behaviour of a Two-Dimensional
Airfoil with a Structural Nonlinearity”, AIAA Journal of Aircraft, Vol. 31, pp. 1395-1401, 1994.
35. M.M. Alishahi and H.
Alighanbari, “Viscous-Inviscid Interactions in Compressible Flow Around
Airfoils”, Iranian Journal of
Science and Technology, Vol. 15, pp. 235-247, 1991.
Refereed
Book Chapter
36. M.R. Amiralaei, H. Alighanbari and S.M.
Hashemi, “Investigation of Low Reynolds Number Unsteady Flow around
Airfoils in Pitching, Plunging and Flapping Motions”, Book title: CFD
Modeling in Development of Renewable Energy Applications, Chapter 7, pp.
261-288, Published by International Energy and Environment Foundation, ISBN 13: 978-1-46623-131-3,
September 2011.
37. H. Alighanbari, M. R. Amiralaei, S. Savtchenko, “Theoretical and Numerical Study of a
Swirling Submerged Jet Flow”, Book title: Engineering Applications of
Computational Fluid Dynamics, Volume 1, Chapter 9, pp. 351-366, Published
by International Energy and Environment Foundation, ISBN 13: 978-1-46623-106-1 ,
September 2011.
38. S. Hashemi and H. Alighanbari, “On the
Dynamics of Rotating Flexible Beam Structures”, Recent Research
Developments in Sound and Vibration, pp. 551-593, 2003.
39. D. Emadi, M. Sahoo, T. Castles and H. Alighanbari, “Prediction of
Mechanical Properties of AS-Cast and Heat-Treated Automotive AL Alloys Using
Artificial Neural Networks”, Light
Metals, pp. 1069-1076, 2001.
Book
Review
40. H. Alighanbari, “Introduction to
Structural Dynamics and Aeroelasticity” by D.H. Hodges and G.A. Pierce, Engineering Dimension, Nov/Dec 2003.
Papers in
Refereed Conference Proceedings
41. M. Melville, A. Kolaei, G. Bramesfeld, and H. Alighanbari “An efficient
model for aeroelastic tailoring of aircraft wings under gust loads”, 2018
AIAA Aerospace Sciences Meeting, 2018.
42. M. Kwong,
F. Xi and H. Alighanbari, "Stability-Based Motion Planning for a Modular
Morphing Wing", SAE 2013 AeroTech Congress
& Exhibition, Canada, Quebec, Montreal, September 2013.
43. B. Raeisi and H.
Alighanbari, "CFD Analysis of Oscillating Blades in Dynamic Stall
Conditions", AERO13 60th Aeronautics Conference and AGM, Canada,
Ontario, Toronto, April 2013.
44. A. Rahimi, K. Raahemifar, K. Kumar, and H. Alighanbari, “Controller
design for rotary inverted pendulum system using particle swarm optimization
algorithm”, 26th IEEE Canadian Conference on Electrical and Computer
Engineering, May 2013.
45. A. Rahimi, K. Kumar K
and H. Alighanbari, "Particle Swarm Optimization Aided Kalman Filter for
Fault Detection, Isolation and Identification of a Reaction Wheel Unit", ASTRO12,
16th CASI Astronautics Conference, Quebec City, April 2012.
46. D.F. Hinz, H. Alighanbari and C. Breitsamter,
“Numerical Simulation of Convective Heat Transfer from a Pitching
NACA0012 Airfoil at Low Reynolds Numbers” Proceedings of AERO 11, 58th
Aeronautics Conference and AGM, Montreal, Canada, April 2011.
47. D.F. Hinz, H. Alighanbari and C. Breitsamter,
“Influence of Heat Transfer on the Aerodynamic Performance of a Pitching
NACA0012 airfoil at Low Reynolds Numbers” Proceedings of AERO 11, 58th
Aeronautics Conference and AGM, Montreal, Canada, April 2011.
48. M.R. Amiralaei, M. Partovibakhsh and H. Alighanbari, “Application of
Adaptive Network-Based Fuzzy Interference System (ANFIS) in Aerodynamics
Prediction of Low-Reynolds-Number Flapping Motion”, IMECE2010-40679,
Proceedings of ASME 2010 International Mechanical Engineering Congress &
Exposition, Vancouver, British Columbia, Nov 2010.
49. M.R. Amiralaei, H.
Alighanbari, “A Parametric Study of a Three Dimensional Pitching Wing
Aerodynamics”, IMECE2010-39400, Proceedings of ASME 2010
International Mechanical Engineering Congress & Exposition, Vancouver,
British Columbia, Nov 2010.
50. M.R. Amiralaei, H.
Alighanbari, and S. Hashemi, “The Unsteady Fluid Dynamics of a Pair of
Pitching Airfoils Using Computational Fluid Dynamics”, IMECE2010-39396,
Proceedings of ASME 2010 International Mechanical Engineering Congress &
Exposition, Vancouver, British Columbia, Nov 2010.
51. M.R. Amiralaei and H.
Alighanbari, “Experimental And Numerical Study
Of A Pitching Blade”, FEDSM-ICNMM2010-31104, Proceedings of ASME 2010 3rd
Joint US-European Fluids Engineering Summer Meeting and 8th International
Conference on Nanochannels, Microchannels,
and Minichannels, August 2-4, 2010, Montreal, Canada.
52. M.R. Amiralaei, H.
Alighanbari, and S. Hashemi, “A Fluid Dynamics Study Of
A Modified Low-Reynolds-Number Flapping Motion”,
FEDSM2010-ICNMM2010-30379, Proceedings of ASME 2010 3rd Joint US-European
Fluids Engineering Summer Meeting and 8th International Conference on Nanochannels, Microchannels, and Minichannels, August 2-4, 2010, Montreal, Canada.
53. H. Alighanbari, M.R.
Amiralaei, and S. Savtchenko, “Theoretical and
Numerical Study of a Swirling Submerged Jet Flow”, FEDSM-ICNMM2010-30777,
Proceedings of ASME 2010 3rd Joint US-European Fluids Engineering Summer
Meeting and 8th International Conference on Nanochannels,
Microchannels, and Minichannels,
August 2-4, 2010, Montreal, Canada
54. M.R. Amiralaei, H.
Alighanbari, and S. Hashemi, “Unsteady CFD of a Plunging Airfoil in
Low-Reynolds-Number Flow Regime”, Paper Number AIAA-2010-4460,
Proceedings of the 40th AIAA Fluid Dynamics Conference, Chicago, Illinois, USA
from 28 June – 1 July 2010.
55. M.R. Amiralaei, H.
Alighanbari, and S. Hashemi, “Unsteady Low-Reynolds-Number Computational
Study of an Airfoil Undergoing a Novel Figure-Eight Kinematics”, Paper
Number AIAA-2010-4457, Proceedings of the 40th AIAA Fluid Dynamics Conference,
Chicago, Illinois, USA from 28 June – 1 July 2010.
56. M.R. Amiralaei, H.
Alighanbari and S. Hashemi, “The Unsteady Aerodynamics of Paired plunging Airfoils Using Computational Fluid Dynamics”,
Paper Number AIAA-2010-8119, Proceedings of AIAA Atmospheric Flight Mechanics
Conference, Toronto, Ontario, Canada, August 2010.
57. M. Adique,
M.R. Amiralaei and H. Alighanbari, “Application of Artificial Neural
Networks in Aerodynamics Prediction of Low-Reynolds-Number Figure-Eight Motion
of an Airfoil”, Paper Number AIAA-2010-8120, Proceedings of AIAA
Atmospheric Flight Mechanics Conference, Toronto, Ontario, Canada, August 2010.
58. M.R. Amiralaei, H.
Alighanbari, and S. Hashemi, “Influence of Unsteady Parameters on the
Aerodynamics of a Low Reynolds Number Pitching Airfoil" 2009 ASME
International Mechanical Engineering Congress & Exposition, Lake Buena
Vista, Florida, November 2009.
59.
S.R.
Borneman, S. Hashemi, H. Alighanbari, “Free Vibration Analysis of Cracked
Stepped Laminated Composite Beams”, 2009 ASME International Mechanical
Engineering Conference & Exhibition, Lake Buena Vista, Florida,
November 2009.
60.
S.
Borneman, S. Hashemi and H. Alighanbari, “A Dynamic Stiffness Element for
Vibration of Cracked Composite Timoshenko Beams,” 12th International
Conference on Civil, Structural and Environmental Eng. Computing, Funchal,
Madeira, Portugal, Sept 2009.
61. M.R. Amiralaei, H.
Alighanbari, and S. Hashemi “Computational Study of Unsteady Very Low
Reynolds Number Flow Around a 2D Pitching Airfoil”, Canadian
Aeronautics and Space Institute AERO’09 Conference, Kanata,
Ontario May 2009.
62.
S.R.
Borneman, S. Hashemi, H. Alighanbari, “A Refined Dynamic Finite Element
for the Aeroelastic Analysis of Tapered Composite Wings”, 17th. Annual
International Conference on Mechanical Engineering, Tehran, Iran, May 2009.
63. S. Borneman, S.
Hashemi, H. Alighanbari, “Free Vibration Analysis of Cracked Composite
Beams: A Dynamic Finite Element”, CD proceedings of the 48th
AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials
Conference, Hawaii, USA, April 2007.
64. S. Borneman, S.
Hashemi, H. Alighanbari, "The Application of Trigonometric Shape Functions
in Vibration Analysis of Cracked Composite Beams", Proceedings of the 6th
Joint Canada-Japan workshop on Composites (Canjap06), Toronto, Canada, August
2006.
65. S. Hashemi, H.
Alighanbari, S. Borneman, "Aeroelastic Analysis of A
Tapered Laminated Composite Wing Using Dynamic Finite Element Modes", The
7th International Conference on Mathematical Problems in Engineering and
Aerospace Sciences (ICNPAA-2006), Budapest, Hungary, June 2006
66. S.R. Borneman, S.
Hashemi and H. Alighanbari, “Coalescence-Type Flutter Analysis of a
Laminated Composite Wing: a Dynamic Finite Element
Formulation”, International Aerospace Conference, Ankara, Turkey, Aug.
2005.
67. E. Texier
and H. Alighanbari , “Dynamic Response of
a Diffuser Pipe Subject to a Harmonic Follower Force”, 20th
Canadian Congress of Applied Mechanics, Montreal, Canada, May 2005.
68. H. Alighanbari,
“Aeroelastic behavior of an airfoil with active flutter suppression
taking into account a structural nonlinearity”, ICNPAA, Fifth
International conference on Mathematical Problems in Engineering and
Aerospace Sciences, Timisoara, Romania, June 2004.
69. S. Hashemi and H.
Alighanbari, "Application of the Dynamic Finite Element Formulation in
Frequency Coalescence Analysis of Laminated Composite Wings", 2nd
International Conference on Fluid Structure Interaction, Cadiz, Spain,
June 2003.
70. M. Borairi
and H. Alighanbari, "Genetic Design of Digital Controllers for Boiler
Level Control in CANDU Reactors", ASME Pressure Vessels and Piping
Conference, Cleveland, Ohio, USA, July 2003.
71. H. Alighanbari,
“Stability and Bifurcations of an Airfoil-Aileron Combination in
Two-Dimensional Incompressible Inviscid Flow”, Proceedings of 43rd
AIAA/ASME/ ASCE/AHS/ASC Structures, Structural Dynamics, and Materials
Conference, Denver, CO, USA, April 2002.
72. H. Alighanbari and S.
Hashemi, “Bifurcation Analysis of an Airfoil Containing a Cubic
Structural Nonlinearity and Subjected to Two-Dimensional Incompressible
Flow”, Proceedings of 43rd AIAA/ASME/ASCE/AHS/ASC Structures,
Structural Dynamics, and Materials Conference, Denver, CO, USA, April 2002.
73. H. Alighanbari,
“Nonlinear Aeroelastic Signal Analysis of an Airfoil-Aileron
Combination”, 23rd ICAS Congress - Toronto, Canada, Sept. 2002.
74. A. Varvani
and H. Alighanbari, “Fatigue Response of Panels in Supersonic flight
speeds”, Eight International Fatigue Congress, Sweden, June 2002.
75. S.M.
Hashemi and H. Alighanbari, “Application of the Dynamic Finite Element
Formulation in Flutter Analysis of Wings”, Proceedings of the Sixth international Conference on Computational Structures
Technology (CST2002), Prague,
Czech Republic, Sept. 2002.
76. S.M. Hashemi and H. Alighanbari, “Frequency Coalescence
Analysis of Wings Using Dynamic Finite Element Formulation”, accepted for
5th International Symposium on
Fluid-Structure Interactions, Aeroelasticity, Flow-Induced Vibration &
Noise, ASME Int'l Mechanical Engineering Congress (IMEC02), New Orleans,
U.S.A, Nov. 2002.
77. H. Alighanbari, “Nonlinear Time Series Analysis of a
Three-DOF Aeroelastic System”, CASI
Aerodynamics Symposium, Toronto, Canada, May 2001.
78. H. Alighanbari and B.H.K. Lee, “Analysis of Nonlinear
Aeroelastic Response”, Proceedings
of 42nd AIAA/ASME/ASCE/AHS/ ASC Structures, Structural Dynamics, and
Materials Conference, Seattle, WA, USA, April 2001.
79. H. Alighanbari, “The Aeroelastic Response of a 3-DOF Airfoil
with Structural Nonlinearities”, Third
International Conference on Nonlinear Problems in Aviation, Daytona Beach,
FL, USA, 2000.
80. H. Alighanbari, Artificial
Neural Networks for Aeromechanical Applications, Report Prepared for
Bombardier Defence Division, pp. 1-68, 1998.
81. H. Alighanbari, C. Semler and M.P. Paidoussis, “A Physical Explanation of the
Destabilizing Effect of Damping for the Pipe Conveying Fluid System”, Proceedings of 16TH
Canadian Congress of Applied Mechanics, 1997.
82. M.P. Paidoussis, C. Semler
and H. Alighanbari, “Physical Explanation of the Destabilizing Effect of
Damping”, Proceedings of 4th
International Symposium on Fluid-Structure Interactions, Aeroelasticity,
Flow-Induced Vibration and Noise, ASME, Aerospace Division (Publication) AD
v 53-2 1997. ASME, Fairfield, NJ, USA. p 29-38
CF: Proceedings of the 1997 ASME
International Mechanical Engineering Congress and Exposition. Part 2 (of 3)
(Dallas, TX, USA)
83. H. Alighanbari and S.J. Price, “Aeroelastic Response of a
Two-Dimensional Airfoil-Aileron Combination with Freeplay
Nonlinearities”, Proceedings of
Sixth Conference on Nonlinear Vibrations, Stability, and Dynamics of
Structures, Blacksburg, VA, USA, 1996.
84. H. Alighanbari and S.J. Price, “Flutter Response of a
Two-Dimensional Airfoil With a Hysteretic Structural
Nonlinearity”, Proceedings of 12TH
Symposium on Engineering Applications of Mechanics, Montreal, Canada, pp.
293-302, 1994.
85. S.J. Price, H. Alighanbari and B.H.K. Lee, “The Aeroelastic
Response of a Two-Dimensional Airfoil with Bilinear and Cubic Structural
Nonlinearities”, Proceedings of 35TH
AIAA/ASME/ASCE/AHS/ ASC Structural Dynamics and Material Conference, Hilton
Head, SC, USA, pp. 1771-1780, 1994.
86. H. Alighanbari and S.J. Price, “Active Flutter Control of a
Two-Dimensional Airfoil With a Structural
Nonlinearity”, Proceedings of 14TH
Canadian Congress of Applied Mechanics, Kingston, Canada, pp. 247-248,
1993.
87. S.J. Price, B.H.K. Lee and H. Alighanbari, “Postinstability Behaviour of a Two-Dimensional Airfoil with
a Structural Nonlinearity”, Proceedings
of 34TH AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and
Material Conference, La Jolla, CA, USA, pp. 1452-1460, 1993.
88. H. Alighanbari and M.M. Alishahi,
“Viscous-Inviscid Interactions in Compressible Flow Around
Airfoils”, Proceedings of the First
Aerodynamics Conference, Tehran, Iran, 1989.