Vibration and Stability Response of Laminated Composite Panels with Elliptical Cutout Under Hygrothermal Conditions
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-99-8986-7_37
Reference24 articles.
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2. Chandra KSS, Rao KV, Rajanna T. A Parametric study on the effect of elliptical cutouts for buckling behavior of composite plates under non-uniform edge loads. Lat Am J Solids Struct. 2020;17(8):1–14. https://doi.org/10.1590/1679-78256225.
3. Savin GN. The stress distribution in a thin shell with an arbitrary hole, problems in cominuum mechanics. Philadelphia, PA, USA; SIAM; 1962, p. 382.
4. Aydin Komur M, Sonmez M. Elastic buckling of rectangular plates under linearly varying in-plane normal load with a circular cutout. Mech Res Commun. 2008;35(6):361–71. https://doi.org/10.1016/j.mechrescom.2008.01.005
5. Rajanna T, Banerjee S, Desai YM, Prabhakara DL. Effect of reinforced cutouts and ply-orientations on buckling behavior of composite panels subjected to non-uniform edge loads. Int J Struct Stab Dyn. 2017; 1850058.
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