Data for: Buckling and postbuckling of advanced grid stiffened truncated conical shells with laminated composite skins
Published: 2 March 2020| Version 2 | DOI: 10.17632/fp46gc7p33.2
Contributors:
Mohammad Ali Kouchakzadeh, Mohammad Noghabi, Mehdi Bohlooly, Babak MirzavandDescription
The closed form formulation of buckling load and postbuckling behavior of advanced grid stiffened conical shells with laminated composite skins are translated to code in MATLAB software. All parameters of structure can be defined and then outputs can be evaluated through this code.
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Mathematics, Aerospace Engineering, Civil Engineering, Mechanical Engineering