Zobrazeno 1 - 10
of 28
pro vyhledávání: '"Chetan K. Hirwani"'
Publikováno v:
Advanced Composite Materials and Structures ISBN: 9781003158813
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1abbdd20c8b8eb3488daea10c1076ac3
https://doi.org/10.1201/9781003158813-16
https://doi.org/10.1201/9781003158813-16
Autor:
Subrata Kumar Panda, Anil K. Lalepalli, Nitin Sharma, Tayfun Dede, Arijit Das, Umut Topal, Chetan K. Hirwani
Publikováno v:
Engineering with Computers. 37:477-487
The bending deflections and the corresponding optimal fiber angle sequences of the subsequent layers have been predicted in this article using a hybrid technique. The structural static responses are computed numerically via the isoparametric finite e
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a141c067a490b214bf90d53ca614c151
https://doi.org/10.1007/s00366-019-00836-8
https://doi.org/10.1007/s00366-019-00836-8
Autor:
Chetan K. Hirwani, Subrata Kumar Panda
Publikováno v:
Engineering with Computers. 36:1201-1214
The nonlinear time-dependent displacement values of the curved (single/doubly) composite debonded shell structure are examined under different kinds of pulse loading in this research. The structural curved panel model is derived mathematically using
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::86bc7498b160ef6b8f27e30d4d9911fa
https://doi.org/10.1007/s00366-019-00757-6
https://doi.org/10.1007/s00366-019-00757-6
Autor:
Subrata Kumar Panda, Chetan K. Hirwani
Publikováno v:
Applied Mathematical Modelling. 65:303-317
Thermoelastic deflection and corresponding stresses of the pre-damaged layered panel structure are investigated numerically in this article including the large deformation kinematics under the linearly varying temperature field. The composite structu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bd8bc8869f995263f24f1b4a3d0c7fc8
https://doi.org/10.1016/j.apm.2018.08.014
https://doi.org/10.1016/j.apm.2018.08.014
Autor:
Chetan K. Hirwani, Hitesh B. Bisen, Brijesh Patel, Subrata Kumar Panda, Rajesh Kumar Satankar, Kulmani Mehar
Publikováno v:
Journal of Natural Fibers. 17:505-519
The natural fiber (Luffa cylindrica fiber) reinforced epoxy composite has been fabricated and their structural responses (frequency and deflection) have been computed experimentally and numerically...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::199647fdb4445e4baf638ef8989a280e
https://doi.org/10.1080/15440478.2018.1503129
https://doi.org/10.1080/15440478.2018.1503129
Publikováno v:
International Journal of Approximate Reasoning. 98:163-176
This is the first-time a higher-order fuzzy finite element model has been proposed and implemented to compute the laminated structural responses (modal frequency and static deflection) numerically including the uncertain elastic properties. The compo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bd200160174849baf76fe54077d4a821
https://doi.org/10.1016/j.ijar.2018.04.013
https://doi.org/10.1016/j.ijar.2018.04.013
Autor:
Subrata Kumar Panda, Chetan K. Hirwani
Publikováno v:
Ocean Engineering. 159:237-252
In the present article, nonlinear static deflections of internally damaged shear deformable laminated composite curved (single and doubly) shell panel are investigated numerically under the quasi-static loading and validated with experimental results
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::20c897be3c17a718f4abb3f5ebea0627
https://doi.org/10.1016/j.oceaneng.2018.04.035
https://doi.org/10.1016/j.oceaneng.2018.04.035
Autor:
Chetan K. Hirwani, Subrata Kumar Panda
Publikováno v:
International Journal of Non-Linear Mechanics. 102:14-24
The influence of the internal debonding on the structural stiffness and the nonlinear modal characteristics of the layered structure are examined extensively in the current research article. For the investigation purpose, the shell frequency response
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::74de67de69c04bbf5c2735cbcb7af314
https://doi.org/10.1016/j.ijnonlinmec.2018.03.005
https://doi.org/10.1016/j.ijnonlinmec.2018.03.005
Publikováno v:
Acta Mechanica. 229:3453-3473
In this article, two types of higher-order kinematic theories are adopted to evaluate the nonlinear bending and the stress values of the internally damaged layered composite flat panel structure numerically including the thickness stretching effect.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::86fcbe227f89fb4b555568882223dea3
https://doi.org/10.1007/s00707-018-2173-8
https://doi.org/10.1007/s00707-018-2173-8
Autor:
Trupti Ranjan Mahapatra, Vijay K. Singh, Subrata Kumar Panda, Chetan K. Hirwani, Kulmani Mehar
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science. 233:1601-1619
In this work, a generic geometrical nonlinear mathematical model of smart composite curved shell panels has been developed for the evaluation of the linear and nonlinear dynamic responses. Further, the dynamic deflections are reduced by employing the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8ed04c76797a8d20aac6f0e7825db8ec
https://doi.org/10.1177/0954406218774362
https://doi.org/10.1177/0954406218774362