S. Ahmad Fazelzadeh

Shiraz University — IR

Engineering · Physical Sciences

34h-index3.2kcitations151works0.02yr avg
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Research Topics

Composite Structure Analysis and Optimization(63), Nonlocal and gradient elasticity in micro/nano structures(50), Aeroelasticity and Vibration Control(42), Vibration and Dynamic Analysis(27), Numerical methods in engineering(21)

Publications151 total

Development and Construction of a Radio-Controlled Aircraft with Distributed Electric Propulsion: Persian Sky-O
Sustainable aviation·2023· 1 cited
In-plane vibration characteristics of metamaterial plates with locally resonant microstructures
Acta Mechanica·2023· 5 cited
Engine Placement Effects on the Flutter of a Medium-Range Box-Wing Aircraft
Journal of Aerospace Engineering·2023· 1 citedOpen Access
Disturbance observer-based adaptive neural guidance and control of an aircraft using composite learning
Control Engineering Practice·2023· 10 citedOpen Access
Flutter Analysis of a 3-D Box Wing with Distributed Electric Propulsion
Sustainable aviation·2023
Experimental and computational physics of fullerenes and their nanocomposites: Synthesis, thermo-mechanical characteristics and nanomedicine applications
Physics Reports·2022· 45 cited
Mechanics of size-dependent materials
Archive of Applied Mechanics·2022· 3 citedOpen Access
Free vibration analysis of curved lattice sandwich beams
Mechanics of Advanced Materials and Structures·2022· 13 citedOpen Access
Free vibration analysis of elastic metamaterial circular curved beams with locally resonant microstructures
Archive of Applied Mechanics·2022· 12 cited
Formation of quasi-static stop band in a new one-dimensional metamaterial
Archive of Applied Mechanics·2022· 13 citedOpen Access
Dynamic stability of rotating cantilever meta-sandwich beam subjected to tangential tip non-conservative force
Applied Mathematical Modelling·2022· 7 cited
Flutter Analysis of a 3D Box-Wing Aircraft Configuration
International Journal of Structural Stability and Dynamics·2021· 5 cited
Flutter Analysis of a 3D Box-Wing Aircraft Configuration
Zenodo (CERN European Organization for Nuclear Research)·2021Open Access
Aeroelastic Stability Analysis of Electric Aircraft Wings with Distributed Electric Propulsors
Aerospace·2021· 17 citedOpen Access
An analytical approach for calculating natural frequencies of finite one-dimensional acoustic metamaterials
Meccanica·2021· 2 cited
One-Dimensional Well-Posed Nonlocal Elasticity Models for Finite Domains
Springer tracts in mechanical engineering·2021· 1 cited
Size-Dependent Continuum Mechanics Approaches
Springer tracts in mechanical engineering·2021· 19 cited
Aeroelastic stability analysis of aircraft wings with initial curvature
Aerospace Science and Technology·2020· 24 citedOpen Access
Review on nonlocal continuum mechanics: Physics, material applicability, and mathematics
Mechanics of Materials·2020· 106 cited
Well-posed nonlocal elasticity model for finite domains and its application to the mechanical behavior of nanorods
Acta Mechanica·2020· 5 cited
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Frequent Co-authors

Esmaeal Ghavanloo(24), S. Pouresmaeeli(6), Mohammad Hosseini(6), Pier Marzocca(6), Hashem Rafii‐Tabar(5), Mohammad Azadi(5), Abbas Mazidi(5), Mohammad Eghtesad(4), E. Azadi(4), H. Kalantari(2), Seid H. Pourtakdoust(2), Mohammad A. Kazemi-Lari(2), Mohamed Shaat(1), P. Malekzadeh(1), P. Zahedinejad(1), Raffaele Barretta(1), Luciano Feo(1), Raimondo Luciano(1), E. Mirzaee(1), Ayesha Kausar(1)