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RISS 인기검색어
- 검색키워드
- 저자 : Chetan Kumar Hirwani (검색결과 4 건)
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Harsh Kumar Pandey,Himanshu Agrawal,Subrata Kumar Panda,Chetan Kumar Hirwani,Pankaj V Katariya,Hukum Chand Dewangan 국제구조공학회 2020 Structural Engineering and Mechanics, An Int'l Jou Vol.73 No.6
The influence on flexural strength of Glass/Epoxy laminated composite curved panels of different geometries (cylindrical, spherical, elliptical, hyperboloid and flat) due to inclusion of nano cenosphere filler examined in this research article. The deflection responses of the hybrid structure are evaluated numerically using the isoparametric finite element technique and modelled mathematically via higher-order displacement structural kinematics. To predict the deflection values, a customised in-house computer code in MATLAB environment is prepared using the higher-order isoparametric formulation. Subsequently, the numerical model validity has been established by comparing with those of available benchmark solution including the convergence characteristics of the finite element solution. Further, a few cenosphere filled hybrid composite are prepared for different volume fractions for the experimental purpose, to review the propose model accuracy. The experimental deflection values are compared with the finite element solutions, where the experimental elastic properties are adopted for the computation. Finally, the effect of different variable design dependent parameter and the percentages of nano cenosphere including the geometrical shapes obtained via a set of numerical experimentation.
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Pandey, Harsh Kumar,Hirwani, Chetan Kumar,Sharma, Nitin,Katariya, Pankaj V.,Dewangan, Hukum Chand,Panda, Subrata Kumar Techno-Press 2019 Advances in nano research Vol.7 No.6
The effect of an increasing percentage of nanofiller (glass cenosphere) with Glass/Epoxy hybrid composite curved panels modeled mathematically using the multiscale concept and subsequent numerical eigenvalues of different geometrical configurations (cylindrical, spherical, elliptical, hyperboloid and flat) predicted in this research article. The numerical model of Glass/Epoxy/Cenosphere is derived using the higher-order polynomial type of kinematic theory in association with isoparametric finite element technique. The multiscale mathematical model utilized for the customized computer code for the evaluation of the frequency data. The numerical model validation and consistency verified with experimental frequency data and convergence test including the experimental elastic properties. The experimental frequencies of the multiscale nano filler-reinforced composite are recorded through the impact hammer frequency test rig including CDAQ-9178 (National Instruments) and LABVIEW virtual programming. Finally, the nano cenosphere filler percentage and different design associated geometrical parameters on the natural frequency data of hybrid composite structural configurations are illustrated through a series of numerical examples.
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B.K. Patle,Chetan K. Hirwani,Subrata Kumar Panda,Pankaj V. Katariya,Hukum Chand Dewangan,Nitin Sharma 국제구조공학회 2020 Steel and Composite Structures, An International J Vol.35 No.6
In this article, the influence of fuzzified uncertain composite elastic properties on non-linear deformation behaviour of the composite structure is investigated under external mechanical loadings (uniform and sinusoidal distributed loading) including the different end boundaries. In this regard, the composite model has been derived considering the fuzzified elastic properties (through a triangular fuzzy function, α cut) and the large geometrical distortion (Green-Lagrange strain) in the framework of the higher-order mid-plane kinematics. The results are obtained using the fuzzified nonlinear finite element model via in-house developed computer code (MATLAB). Initially, the model accuracy has been established and explored later to show the dominating elastic parameter affect the deflection due to the inclusion of fuzzified properties by solving a set of new numerical examples.
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Pankaj V. Katariya,Subrata Kumar Panda,Chetan Kumar Hirwani 한국섬유공학회 2022 Fibers and polymers Vol.23 No.11
The large geometrical distortion effect on the skew sandwich panel and improvement of the eigenvalue responsesdue to the embedded functional material (shape memory alloy, SMA) is investigated for the first time in this research. Thestructural responses are numerically predicted via a macro-mechanical nonlinear finite element model with the alternatingelastic constants due to the change in environmental conditions. The nonlinear formulation is derived mathematically viathird-order deformation kinematics including the through-thickness elongations. Moreover, the large geometrical shapechanges of the skew sandwich shell panels are described by Green-Lagrange strain whereas the material nonlinearity due tothe functional fibre inclusion modelled through the step-wise temperature-dependent properties of the individual panelconstituents (face skins, core and SMA fibre). The proposed macro-mechanical material model is helping to evaluate thecomposite sandwich properties due to the variation of hygrothermal environment. The eigenvalue type of system equation isderived through variation principle with and without excess geometrical alteration and solved via the robust Picard’s iterationtechnique in association with nonlinear finite element steps. The marching technique is adopted to include the materialnonlinearity within the mathematical model to include the variation of SMA elastic properties (volume fraction, pre-strainand blocking stress). The viability of the proposed model to compute the responses are tested by checking a few examplesconsidering the curvature parameter, layer sequence, SMA layer and the environmental changes. Additionally, it is extendedto figure out the influences of individual and combined cases of parameters on the nonlinear frequency and bucklingcharacteristics of SMA bonded sandwich shell panel with and without skew angle.
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