M
Mostafa Talebitooti
Researcher at University of Qom
Publications - 29
Citations - 401
Mostafa Talebitooti is an academic researcher from University of Qom. The author has contributed to research in topics: Conical surface & Boundary value problem. The author has an hindex of 9, co-authored 27 publications receiving 258 citations. Previous affiliations of Mostafa Talebitooti include Iran University of Science and Technology & Isfahan University of Technology.
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Free vibrations of rotating composite conical shells with stringer and ring stiffeners
TL;DR: In this paper, an analytical solution for the free vibration of rotating composite conical shells with axial stiffeners (stringers) and circumferential stiffener (rings), is presented using an energy-based approach.
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Three-dimensional free vibration analysis of rotating laminated conical shells: layerwise differential quadrature (LW-DQ) method
TL;DR: In this paper, a free vibration analysis of rotating conical shells with different boundary conditions based on the layerwise differential quadrature method (LW-DQM) is presented.
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Thermal buckling and free vibration of FG truncated conical shells with stringer and ring stiffeners using differential quadrature method
TL;DR: In this article, the thermal buckling and free vibration of orthogonally stiffened functionally graded truncated conical shells in thermal environment is investigated, where the conical shell has been stiffened by orthogonal stiffening.
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A semi-analytical approach on the effect of external lateral pressure on free vibration of joined sandwich aerospace composite conical-conical shells
TL;DR: In this paper, the free vibrational behavior of composite sandwich conical-conical shells under external lateral pressure was investigated by applying Hamilton's principle and considering initial mechanical stresses solved by static equilibrium equations.
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Free vibration and critical speed of moderately thick rotating laminated composite conical shell using generalized differential quadrature method
TL;DR: In this article, a generalized differential quadrature (GDQM) method is employed to consider the free vibration and critical speed of moderately thick rotating laminated composite conical shells with different boundary conditions developed from the first-order shear deformation theory (FSDT).