Please use this identifier to cite or link to this item: https://idr.nitk.ac.in/jspui/handle/123456789/15646
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dc.contributor.authorTwinkle C.M.
dc.contributor.authorNithun C.
dc.contributor.authorPitchaimani J.
dc.contributor.authorRajamohan V.
dc.date.accessioned2021-05-05T10:27:35Z-
dc.date.available2021-05-05T10:27:35Z-
dc.date.issued2020
dc.identifier.citationProceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science Vol. , , p. -en_US
dc.identifier.urihttps://doi.org/10.1177/0954406220936738
dc.identifier.urihttp://idr.nitk.ac.in/jspui/handle/123456789/15646-
dc.description.abstractIn this study, experimental investigations carried out to analyze the influences of different in-plane temperature variations on buckling and free vibration responses of metal and fiber-reinforced laminated composite cylindrical panels are presented. Initially, critical buckling temperature is calculated then free vibration analysis is performed as a function of the buckling temperature to analyze the changes in the natural frequencies and mode shapes. Experimental results revealed that the thermal buckling strength of the panel is significantly influenced by the nature of the heating condition. Similarly, significant changes in free vibration mode shapes are observed with the rise in temperature and also according to the heating conditions. It is also observed that, with the increase in temperature, nodal and anti-nodal lines of free vibration modes shifting towards the heating source. The experimental results are compared with the numerical simulation for the studies on the isotropic cylindrical panel and both the results are in good agreement. © IMechE 2020.en_US
dc.titleModal analysis of cylindrical panels at elevated temperatures under nonuniform heating conditions: Experimental investigationen_US
dc.typeArticleen_US
Appears in Collections:1. Journal Articles

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