Zobrazeno 1 - 10
of 15
pro vyhledávání: '"Vahid Khalafi"'
Autor:
Vahid Khalafi, Jamshid Fazilati
Publikováno v:
Journal of Theoretical and Applied Vibration and Acoustics, Vol 4, Iss 2, Pp 171-188 (2018)
A NURBS-based isogeometric finite element formulation is developed and adopted to the free vibration analysis of finite square and skew laminated plates. Variable stiffness plies are assumed due to implementation of curvilinear fiberreinforcements. I
Externí odkaz:
https://doaj.org/article/8bd6a99716664c53beee4cebf5fca204
Publikováno v:
International Journal of Applied Mechanics. 15
In this study, a cubic NURBS-based isogeometric finite element method is developed to study the aeroelastic tailoring of variable stiffness composite laminated (VSCL) plates, including skew, skew-tapered, tapered, and circular shapes based on third-o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::de0ea25f829dc916e2b11ea9268d773f
https://doi.org/10.1142/s1758825122500910
https://doi.org/10.1142/s1758825122500910
Autor:
Vahid Khalafi, Jamshid Fazilati
Publikováno v:
Chinese Journal of Aeronautics, Vol 34, Iss 1, Pp 266-280 (2021)
The bonded repair techniques seem to be the most frequent procedures in the aviation maintenance. The achieved composite repaired perforated thin-walled plate is a complex geometry with high numerical analysis cost. The NURBS-based Isogeometric Analy
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::984670450b9f9ddc31a29707935e02fa
https://doi.org/10.1016/j.cja.2020.09.038
https://doi.org/10.1016/j.cja.2020.09.038
Publikováno v:
International Journal of Applied Mechanics. 13
In this study, the optimization of free vibration and flutter analysis of a composite plate with the implementation of different boundary conditions is investigated. The governing equations of a composite plate are obtained using the first shear defo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f1464c80074e1f1f20813c37896c7ebb
https://doi.org/10.1142/s1758825121500903
https://doi.org/10.1142/s1758825121500903
Publikováno v:
Thin-Walled Structures. 179:109638
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::725881e3aa1c821a2c3ad5c8ae1316af
https://doi.org/10.1016/j.tws.2022.109638
https://doi.org/10.1016/j.tws.2022.109638
Publikováno v:
Energy Conversion and Management. 196:581-590
One of the main challenges of employing lithium-ion batteries specially in large-scale applications is overheating due to the heat generation. In this work, the effect of using Potassium Polyacrylate, a superabsorbent hydrogel, on decrease in the max
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ecdd8b49eb456748dfb89edcec055a0f
https://doi.org/10.1016/j.enconman.2019.06.043
https://doi.org/10.1016/j.enconman.2019.06.043
Autor:
Vahid Khalafi, Jamshid Fazilati
Publikováno v:
Journal of Reinforced Plastics and Composites. 38:885-895
The optimization of linear flutter behavior of the thin plates made from tow-steered fiber-reinforced laminates is investigated. In the tow-steered variable stiffness composite laminates, the fiber...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d65ad68fff654fabbd908bbbd3827956
https://doi.org/10.1177/0731684419854800
https://doi.org/10.1177/0731684419854800
Autor:
Vahid Khalafi, Jamshid Fazilati
Publikováno v:
Thin-Walled Structures. 133:96-105
For the first time, the parametric instability regions of variable stiffness laminated composite quadrilateral plates subjected to uniform in-plane loadings are studied. The static as well as time-varying inplane loadings are assumed distributed thro
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::00e9dd07a7d83af1a33a8b6307df063a
https://doi.org/10.1016/j.tws.2018.09.035
https://doi.org/10.1016/j.tws.2018.09.035
Autor:
Jamshid Fazilati, Vahid Khalafi
Publikováno v:
Journal of Fluids and Structures. 82:198-214
An enhanced isogeometric finite element method is developed to investigate the free vibration analysis as well as the linear flutter characteristics of finite square as well as skew laminated plates. The laminates are assumed composed of variable sti
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::db4734495d3e35f1ce41413b75432699
https://doi.org/10.1016/j.jfluidstructs.2018.07.002
https://doi.org/10.1016/j.jfluidstructs.2018.07.002
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 233:1715-1727
In the present paper, the aero-thermo-elastic behavior of a finite (three-dimensional) cylindrical curved panel geometry made from functionally graded material under high supersonic airflow is investigated. A generalized differential quadrature formu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bd0e498148618c5408c7caa2eb2b4e7d
https://doi.org/10.1177/0954410018763861
https://doi.org/10.1177/0954410018763861