IZADI, Mohammad Hadi ;SHAHROKH, Hosseini Hashemi ;HABIBNEJAD KORAYEM, Moharam . Buckling of Joined Composite Conical Shells Using Shear Deformation Theory under Axial Compression. Strojniški vestnik - Journal of Mechanical Engineering, [S.l.], v. 65, n.10, p. 574-584, october 2019. ISSN 0039-2480. Available at: <https://www.sv-jme.eu/sl/article/buckling-of-joined-composite-conical-shells-using-shear-deformation-theory-under-axial-compression/>. Date accessed: 20 dec. 2024. doi:http://dx.doi.org/10.5545/sv-jme.2019.6146.
Izadi, M., Shahrokh, H., & Habibnejad Korayem, M. (2019). Buckling of Joined Composite Conical Shells Using Shear Deformation Theory under Axial Compression. Strojniški vestnik - Journal of Mechanical Engineering, 65(10), 574-584. doi:http://dx.doi.org/10.5545/sv-jme.2019.6146
@article{sv-jmesv-jme.2019.6146,
author = {Mohammad Hadi Izadi and Hosseini Hashemi Shahrokh and Moharam Habibnejad Korayem},
title = {Buckling of Joined Composite Conical Shells Using Shear Deformation Theory under Axial Compression},
journal = {Strojniški vestnik - Journal of Mechanical Engineering},
volume = {65},
number = {10},
year = {2019},
keywords = {buckling; joined laminated conical shell; first-order shear deformation; power series},
abstract = {This paper investigates critical buckling loads in joined conical shells under axial compression. An analytical approach has been applied to study classical linear buckling of joined cones that are made of cross-ply fiber reinforced laminates. The governing equations have been extracted using first-order shear deformation theory (FSDT), and an analytical solution has been applied to extract critical buckling loads. Accordingly, the system of partial differential equations has been solved via separation of variables using Fourier expansion and power series method. The effects of the number of layers, lamination sequences, semi-vertex angles, shell thicknesses, shell lengths and boundary conditions on the stability of joined cones have been examined. For validation, the specific examples of the present study have been compared to previous studies. Using ABAQUSE/CAE software (a FEM-based software), the results of finite element have been extracted. The present method is in good agreement with the finite element and other research results. Finally, the differences in classical shell theory (CST) of Donnell type and first-order shear deformation theory have been discussed for different shell thicknesses.},
issn = {0039-2480}, pages = {574-584}, doi = {10.5545/sv-jme.2019.6146},
url = {https://www.sv-jme.eu/sl/article/buckling-of-joined-composite-conical-shells-using-shear-deformation-theory-under-axial-compression/}
}
Izadi, M.,Shahrokh, H.,Habibnejad Korayem, M. 2019 October 65. Buckling of Joined Composite Conical Shells Using Shear Deformation Theory under Axial Compression. Strojniški vestnik - Journal of Mechanical Engineering. [Online] 65:10
%A Izadi, Mohammad Hadi %A Shahrokh, Hosseini Hashemi %A Habibnejad Korayem, Moharam %D 2019 %T Buckling of Joined Composite Conical Shells Using Shear Deformation Theory under Axial Compression %B 2019 %9 buckling; joined laminated conical shell; first-order shear deformation; power series %! Buckling of Joined Composite Conical Shells Using Shear Deformation Theory under Axial Compression %K buckling; joined laminated conical shell; first-order shear deformation; power series %X This paper investigates critical buckling loads in joined conical shells under axial compression. An analytical approach has been applied to study classical linear buckling of joined cones that are made of cross-ply fiber reinforced laminates. The governing equations have been extracted using first-order shear deformation theory (FSDT), and an analytical solution has been applied to extract critical buckling loads. Accordingly, the system of partial differential equations has been solved via separation of variables using Fourier expansion and power series method. The effects of the number of layers, lamination sequences, semi-vertex angles, shell thicknesses, shell lengths and boundary conditions on the stability of joined cones have been examined. For validation, the specific examples of the present study have been compared to previous studies. Using ABAQUSE/CAE software (a FEM-based software), the results of finite element have been extracted. The present method is in good agreement with the finite element and other research results. Finally, the differences in classical shell theory (CST) of Donnell type and first-order shear deformation theory have been discussed for different shell thicknesses. %U https://www.sv-jme.eu/sl/article/buckling-of-joined-composite-conical-shells-using-shear-deformation-theory-under-axial-compression/ %0 Journal Article %R 10.5545/sv-jme.2019.6146 %& 574 %P 11 %J Strojniški vestnik - Journal of Mechanical Engineering %V 65 %N 10 %@ 0039-2480 %8 2019-10-17 %7 2019-10-17
Izadi, Mohammad Hadi, Hosseini Hashemi Shahrokh, & Moharam Habibnejad Korayem. "Buckling of Joined Composite Conical Shells Using Shear Deformation Theory under Axial Compression." Strojniški vestnik - Journal of Mechanical Engineering [Online], 65.10 (2019): 574-584. Web. 20 Dec. 2024
TY - JOUR AU - Izadi, Mohammad Hadi AU - Shahrokh, Hosseini Hashemi AU - Habibnejad Korayem, Moharam PY - 2019 TI - Buckling of Joined Composite Conical Shells Using Shear Deformation Theory under Axial Compression JF - Strojniški vestnik - Journal of Mechanical Engineering DO - 10.5545/sv-jme.2019.6146 KW - buckling; joined laminated conical shell; first-order shear deformation; power series N2 - This paper investigates critical buckling loads in joined conical shells under axial compression. An analytical approach has been applied to study classical linear buckling of joined cones that are made of cross-ply fiber reinforced laminates. The governing equations have been extracted using first-order shear deformation theory (FSDT), and an analytical solution has been applied to extract critical buckling loads. Accordingly, the system of partial differential equations has been solved via separation of variables using Fourier expansion and power series method. The effects of the number of layers, lamination sequences, semi-vertex angles, shell thicknesses, shell lengths and boundary conditions on the stability of joined cones have been examined. For validation, the specific examples of the present study have been compared to previous studies. Using ABAQUSE/CAE software (a FEM-based software), the results of finite element have been extracted. The present method is in good agreement with the finite element and other research results. Finally, the differences in classical shell theory (CST) of Donnell type and first-order shear deformation theory have been discussed for different shell thicknesses. UR - https://www.sv-jme.eu/sl/article/buckling-of-joined-composite-conical-shells-using-shear-deformation-theory-under-axial-compression/
@article{{sv-jme}{sv-jme.2019.6146},
author = {Izadi, M., Shahrokh, H., Habibnejad Korayem, M.},
title = {Buckling of Joined Composite Conical Shells Using Shear Deformation Theory under Axial Compression},
journal = {Strojniški vestnik - Journal of Mechanical Engineering},
volume = {65},
number = {10},
year = {2019},
doi = {10.5545/sv-jme.2019.6146},
url = {https://www.sv-jme.eu/sl/article/buckling-of-joined-composite-conical-shells-using-shear-deformation-theory-under-axial-compression/}
}
TY - JOUR AU - Izadi, Mohammad Hadi AU - Shahrokh, Hosseini Hashemi AU - Habibnejad Korayem, Moharam PY - 2019/10/17 TI - Buckling of Joined Composite Conical Shells Using Shear Deformation Theory under Axial Compression JF - Strojniški vestnik - Journal of Mechanical Engineering; Vol 65, No 10 (2019): Strojniški vestnik - Journal of Mechanical Engineering DO - 10.5545/sv-jme.2019.6146 KW - buckling, joined laminated conical shell, first-order shear deformation, power series N2 - This paper investigates critical buckling loads in joined conical shells under axial compression. An analytical approach has been applied to study classical linear buckling of joined cones that are made of cross-ply fiber reinforced laminates. The governing equations have been extracted using first-order shear deformation theory (FSDT), and an analytical solution has been applied to extract critical buckling loads. Accordingly, the system of partial differential equations has been solved via separation of variables using Fourier expansion and power series method. The effects of the number of layers, lamination sequences, semi-vertex angles, shell thicknesses, shell lengths and boundary conditions on the stability of joined cones have been examined. For validation, the specific examples of the present study have been compared to previous studies. Using ABAQUSE/CAE software (a FEM-based software), the results of finite element have been extracted. The present method is in good agreement with the finite element and other research results. Finally, the differences in classical shell theory (CST) of Donnell type and first-order shear deformation theory have been discussed for different shell thicknesses. UR - https://www.sv-jme.eu/sl/article/buckling-of-joined-composite-conical-shells-using-shear-deformation-theory-under-axial-compression/
Izadi, Mohammad Hadi, Shahrokh, Hosseini Hashemi, AND Habibnejad Korayem, Moharam. "Buckling of Joined Composite Conical Shells Using Shear Deformation Theory under Axial Compression" Strojniški vestnik - Journal of Mechanical Engineering [Online], Volume 65 Number 10 (17 October 2019)
Strojniški vestnik - Journal of Mechanical Engineering 65(2019)10, 574-584
© The Authors, CC-BY 4.0 Int. Change in copyright policy from 2022, Jan 1st.
This paper investigates critical buckling loads in joined conical shells under axial compression. An analytical approach has been applied to study classical linear buckling of joined cones that are made of cross-ply fiber reinforced laminates. The governing equations have been extracted using first-order shear deformation theory (FSDT), and an analytical solution has been applied to extract critical buckling loads. Accordingly, the system of partial differential equations has been solved via separation of variables using Fourier expansion and power series method. The effects of the number of layers, lamination sequences, semi-vertex angles, shell thicknesses, shell lengths and boundary conditions on the stability of joined cones have been examined. For validation, the specific examples of the present study have been compared to previous studies. Using ABAQUSE/CAE software (a FEM-based software), the results of finite element have been extracted. The present method is in good agreement with the finite element and other research results. Finally, the differences in classical shell theory (CST) of Donnell type and first-order shear deformation theory have been discussed for different shell thicknesses.