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Ehsan Selahi
Ehsan Selahi
Assistant Professor, Islamic Azad University, Marvdasht Branch, Marvdasht, Iran
Verified email at miau.ac.ir
Title
Cited by
Cited by
Year
Transient dynamic and free vibration analysis of functionally graded truncated conical shells with non-uniform thickness subjected to mechanical shock loading
AR Setoodeh, M Tahani, E Selahi
Composites Part B: Engineering 43 (5), 2161-2171, 2012
712012
Hybrid layerwise-differential quadrature transient dynamic analysis of functionally graded axisymmetric cylindrical shells subjected to dynamic pressure
AR Setoodeh, M Tahani, E Selahi
Composite Structures 93 (11), 2663-2670, 2011
572011
Analytical solution of stress field in adhesively bonded composite single-lap joints under mechanical loadings
SA Yousefsani, M Tahani, E Selahi
International Journal of Engineering 27 (3), 475-486, 2014
242014
Three-dimensional transient analysis of functionally graded truncated conical shells with variable thickness subjected to an asymmetric dynamic pressure
E Selahi, AR Setoodeh, M Tahani
International Journal of Pressure Vessels and Piping 119, 29-38, 2014
212014
Failure study of hybrid bonded-bolted composite single and double lap joints
E Selahi
Journal of Stress Analysis 3 (2), 37-46, 2019
122019
Elasticity solution of adhesive tubular joints in laminated composites with axial symmetry
E Selahi
Archive of Mechanical Engineering 65 (3), 441-456, 2018
82018
Non-linear analysis of adhesive joints in composite structures
E Selahi
ADMT Journal 9 (1), 2016
72016
Three-dimensional transient analysis of functionally graded cylindrical shells subjected to asymmetric dynamic pressure
M Tahani, AR Setoodeh, E Selahi
Science and Engineering of Composite Materials 20 (1), 75-85, 2013
62013
Crack initiation and growth simulations of functionally graded dental implant subjected to cyclic axial loads
A Mohammadi Anari, E Selahi
Fatigue & Fracture of Engineering Materials & Structures 45 (11), 3123-3136, 2022
32022
Mathematical modeling of composite single scarf adhesive joint
E Selahi, I Rajabi, MH Kadivar
13th. International Mechanical Engineering Conference, Isfahan, Iran, 2005
32005
Analysis of adhesive double strap joint for composite materials
E Selahi, I Rajabi, M Behzadi, MH and Kadivar
International Conference on Recent Advances in Composite Materials, 2004
32004
Analysis of adhesive double lap joint for composite materials
E Selahi, I Rajabi, M Behzadi, MH Kadivar
International Conference on Recent Advances in Composite Materials, Varanasi …, 2004
32004
Damage evaluation of protected and non-protected composite sandwich panels with insulation subjected to fire and impact loads
A Sepehri, E Selahi
Iranian Journal of Science and Technology, Transactions of Mechanical …, 2020
22020
Transient Analysis of Functionally Graded Cylindrical Shells Subjected to Asymmetric Thermo-mechanical Shock Loads with Temperature Dependent Material Properties
E Selahi, AR Setoodeh, M Tahani
Journal of Solid and Fluid Mechanics 9 (2), 153-166, 2019
22019
Performance analysis of bone scaffolds with carbon nanotubes, barium titanate particles, hydroxyapatite and polycaprolactone
A Osfoori, E Selahi
Biomaterials and Biomechanics in Bioengineering 4 (1), 33-44, 2019
22019
Stress Analysis of Adhesively Bonded Joints in Composite Structures
E Selahi
Master of Science thesis, Shiraz University, Shiraz, Iran, 2004
22004
Failure analysis of fiberglass‐vinyl ester composite cylinders subjected to fire and asymmetric transient pressure
E Selahi, AR Setoodeh, M Tahani
Polymer Composites 42 (10), 5607-5623, 2021
12021
Transient Analysis and Free Vibration of Functionally Graded Truncated Conical Shells Subjected to Moving Pressure
E Selahi, AR Setoodeh, M Tahani
Amirkabir Journal of Mechanical Engineering 53 (2), 897-912, 2021
12021
Semi Analytical Transient Dynamic Analysis of Composite Adhesive Single-lap Joints
E Selahi
Mechanics of Advanced Composite Structures 7 (1), 137-145, 2020
12020
Fatigue life assessment of composite airplane wing subjected to variable mechanical and thermal loads
A Ebadi, E Selahi
Journal of Aerospace Science and Technology 11 (2), 1-11, 2017
12017
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