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Babak Mirzavand
Academic Rank : Associate Professor
Faculty of New Science and Technology
Aerospace Engineering
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473
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14
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as of :
2025-05-01
560
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14
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as of :
2025-05-05
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Scholarly Works
2005
2024
473
Citations
14
h-Index
33
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2
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2024
1. Characterization of elastic modulus and fracture toughness of randomly oriented chopped glass fibers functionally graded materials
Izadi Sayed Mohammad Hossein,
Fakoorsaghieh Mehdi
,
Mirzavand Babak
(2024)., STEEL AND COMPOSITE STRUCTURES, 53(1).
2. A novel mixed mode fracture criterion for functionally graded materials considering fracture process zone
Izadi Sayed Mohammad Hossein,
Fakoorsaghieh Mehdi
,
Mirzavand Babak
(2024)., THEORETICAL AND APPLIED FRACTURE MECHANICS, 134(104710), 104710.
2022
1. Effect of temperature and magnetoelastic loads on the free vibration of a sandwich beam with magnetorheological core and functionally graded material constraining layer
Mirzavand Babak
,
Shams Shahrokh
, Kazemi Mohammad Reza, Rokn-Abadi Mohammad (2022)., ACTA MECHANICA, 234(234).
2. On Thermally Induced Vibration Control of Hybrid Magnetostrictive Beams and Plates
Mirzavand Babak
, Javadi Mohammad-Ghasem,
Amiri Atashgah Mohammad-ali
(2022)., International Journal of Structural Stability and Dynamics, Online(-).
3. Closed form solutions for thermo-mechanical buckling analysis of shallow piezo-laminated spherical shells
Mirzavand Babak
, Feyz Mohammadreza, Asnaashari Amirmasoud (2022)., MECHANICS BASED DESIGN OF STRUCTURES AND MACHINES, 1(1), 1-25.
2021
1. Nonlinear stress analysis of shell structures in buckling and snapping problems by exact geometry solid-shell elements through sampling surfaces formulation
Kulikov Gennady M., Bohlooly Mehdi, Plotnikova Svetlana V., Kouchakzadeh Mohammad Ali,
Mirzavand Babak
(2021)., INTERNATIONAL JOURNAL OF NON-LINEAR MECHANICS, 129(1), 103661.
2020
1. Cubic static stall model for nonlinear aeroelastic behavior of high-aspect-ratio flexible composite wings
Shams Shahrokh
, Kazemi Mohammad Reza,
Mirzavand Babak
(2020)., Journal of the Brazilian Society of Mechanical Sciences and Engineering, 42(12), 627.
2. Dynamic instability characteristics of advanced grid stiffened conical shell with laminated composite skins
Bohlooly Mehdi, Kouchakzadeh Mohammad Ali,
Mirzavand Babak
, Noghabi Mohammad (2020)., JOURNAL OF SOUND AND VIBRATION, 488(1), 115572.
3. Torsional Aeroelasticity of a Flexible VAWT Blade using a Combined Aerodynamic Method by Considering Post-stall and Local Reynolds Regime
Shams Shahrokh
, Molaei Ahad,
Mirzavand Babak
(2020)., Journal of Applied and Computational Mechanics, 6(4).
4. Buckling and postbuckling of advanced grid stiffened truncated conical shells with laminated composite skins
Bohlooly Mehdi, Kouchakzadeh Mohammad Ali,
Mirzavand Babak
, Noghabi Mohammad (2020)., THIN-WALLED STRUCTURES, 149(01), 106528.
2019
1. Impact of Blade Aeroelastic Torsion on the Performance of VAWT Using a Innovative Combined Nonlinear Aerodynamic Method
Shams Shahrokh
, Molaei Ahad,
Mirzavand Babak
(2019)., Journal of Mechanical Engineering Research and Developments, 1(1).
2. Higher-order stability analysis of imperfect laminated piezo-composite plates on elastic foundations under electro-thermo-mechanical loads
Mirzavand Babak
, Bohlooly Mehdi (2019)., Journal of Solid Mechanics in Engineering, 11(3).
3. Post-buckling analysis of non-uniformly heated functionally graded cylindrical shells enhanced by shape memory alloys using classical lamination theory
Mirzavand Babak
, Pourmohammad Hamid (2019)., JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 30(16), 2421-2435.
2018
1. An analytical approach for postbuckling of eccentrically or concentrically stiffened composite double curved panel on nonlinear elastic foundation
Bohlooly Mehdi,
Mirzavand Babak
, Malekzadeh Fard Keramat (2018)., APPLIED MATHEMATICAL MODELLING, 62(62), 415-435.
2. Kinematic analysis of articulated flapping wings mechanisms considering nonlinear quasi-steady aerodynamic
Shams Shahrokh
,
Mirzavand Babak
, Mansoori Seyyed Mohammad, Kazemi Mohammadreza (2018)., Mechanical Engineering modares, 17(12), 87.
2017
1. Cubic Static Stall Model for Aeroelastic Behavior of Composite Blade
Shams Shahrokh
, Kazemi Mohammadreza,
Mirzavand Babak
(2017)., 1st International Symposium on Wind and Tidal Power (ISWTP 2017),28-31 May 2017, 28-31 May, Montreal, Canada.
2. Thermally induced Vibrations of Functionally Graded Beams Using HSDT
Ghasemi Hamed,
Mirzavand Babak
(2017)., 16th International Conference of Iranian Aerospace Society (AERO 2017), 21-23 February, Tehran, Iran.
3. Investigation of nonlinear aeroelastic behavior of airfoils with flow separation based on cubic static stall modeling
Shams Shahrokh
, Kazemi Mohammadreza,
Mirzavand Babak
, Khojasteh_bakhteh_koupaie Zahra (2017)., Mechanical Engineering modares, 16(12), 311.
2016
1. Postbuckling and deflection response of imperfect piezo-composite plates resting on elastic foundations under in-plane and lateral compression and electro-thermal loading
Bohlooly Mehdi,
Mirzavand Babak
(2016)., MECHANICS OF ADVANCED MATERIALS AND STRUCTURES, 25(3), 1-10.
2. Thermomechanical buckling of hybrid cross-ply laminated rectangular plates
Bohlooly Mehdi,
Mirzavand Babak
(2016)., ADVANCED COMPOSITE MATERIALS, 26(5), 1-20.
3. Hydroelastic coupled vibrations in spherical containers of membrane bottom, partially filled with frictionless liquids
Cheraghi Behnam,
Mirzavand Babak
,
Shafaei Mazyar
(2016)., Mechanical Engineering modares, 16(4), 155-162.
2015
1. Thermal Buckling of Piezolaminated Plates Subjected to Different Loading Conditions
Mirzavand Babak
, Bohlooly Mehdi (2015)., JOURNAL OF THERMAL STRESSES, 38(10), 1140-1164.
2. Thermal buckling of shallow/nonshallow piezoelectric-composite cylindrical shells
Mirzavand Babak
, Rezapour Pedram, Bohlooly Mehdi (2015)., MECHANICS OF ADVANCED MATERIALS AND STRUCTURES, 23(10), 1-33.
3. Closed form solutions for buckling and postbuckling analysis of imperfect laminated composite plates with piezoelectric actuators
Bohlooly Mehdi,
Mirzavand Babak
(2015)., COMPOSITES PART B-ENGINEERING, 72(1359-8368), 21-29.
4. A Closed-Form Solution for Thermal Buckling of Cross-Ply Piezolaminated Plates
Bohlooly Mehdi,
Mirzavand Babak
(2015)., International Journal of Structural Stability and Dynamics, 16(0219-4554), 1450112.
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