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Państwowej Szkoły Wyższej w Białej Podlaskiej

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Zapytanie: PLATES
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Nr opisu: ness is assumed and the use of the shear correction factor is avoided. A C0 finite element formulation of the mathematical model is developed to analyze the dynamic behavior of laminated composite twisted plate with cutout and additional mass. Given that no results on the present problem of free vibration of laminated composite twisted plate with cutout and additional mass are available in literature, novel results for different twist angles of laminated composite plates along with mode shapes are presented by varying the geometry, boundary conditions, and ply orientations.^acutout^afree vibration^aplates^amode shape
Autorzy: .
Tytuł pracy:
Charakterystyka formalna: rough the plate thickness is assumed and the use of the shear correction factor is avoided. A C0 finite element formulation of the mathematical model is developed to analyze the dynamic behavior of laminated composite twisted plate with cutout and additional mass. Given that no results on the present problem of free vibration of laminated composite twisted plate with cutout and additional mass are available in literature, novel results for different twist angles of laminated composite plates along with mode shapes are presented by varying the geometry, boundary conditions, and ply orientations.^acutout^afree vibration^aplates^amode shape
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Nr opisu: T-Reinforced Rhombic Laminates00000358440000001767AOartykuł oryginalny naukowyPUBLIKACJAPEŁNA PUBLIKACJAAAartykuł w czasopiśmie z IF (wykaz MNiSW)AFILIACJA PODANAENGhttp://www.mdpi.com/2076-3417/8/5/834PRACA RECENZOWANA100^a2076-3417^bA^gABC^iX^jXY^a003^b003^c2018-09-11, 10:23^d2019-09-25, 12:23^e3621939216^f3521799016^aStatic and Dynamic Response of FG-CNT-Reinforced Rhombic Laminates^aApplied Sciences^a2018^bVol. 8^cissue 5^darticle number 834^a2076-3417^a2017/2018^a10.3390/app8050834^aAndrzejuk, Wojciech^cy^aplates^bdziałalność statutowa WNET PSW^c2017-WNET/KNT/ZB/1^aFINAL_PUBLISHED^bCC-BY^cAT_PUBLICATION^eOPEN_JOURNAL^aThe present study focuses on the static and dynamic response of functionally graded carbon nanotube (FG-CNT)-reinforced rhombic laminates. The cubic variation of thickness coordinate in the displacement field is considered in terms of Taylor's series expansion, which represents the higher-order transverse cross-sectional deformation modes. The condition of zero-transverse shear strain at upper and lower surface of FG-CNT-reinforced rhombic laminates is imposed in the present formulation. The present two-dimensional model is formulated in a finite element, with the C0 element consisting of seven nodal unknowns per node. The final material properties of FG-CNT-reinforced rhombic laminates are estimated using the rule of mixture. The obtained numerical are compared with the results available in the literature to verify the reliability of the present model. The present study investigates the effect of CNT distribution, loading pattern, volume fraction, and various combinations of boundary constraints by developing a finite element code in FORTRAN.^acarbon nanotubes^astructure^askew^afinite element method^adeflection^afrequency
Autorzy: , , A 003 Vol. 8 działalność statutowa WNET PSW CC-BY 2076-3417003Static and Dynamic Response of FG-CNT-Reinforced Rhombic LaminatesApplied Sciences20182076-34172017/201810.3390/app8050834Andrzejuk, WojciechplatesFINAL_PUBLISHEDThe present study focuses on the static and dynamic response of functionally graded carbon nanotube (FG-CNT)-reinforced rhombic laminates. The cubic variation of thickness coordinate in the displacement field is considered in terms of Taylor's series expansion, which represents the higher-order transverse cross-sectional deformation modes. The condition of zero-transverse shear strain at upper and lower surface of FG-CNT-reinforced rhombic laminates is imposed in the present formulation. The present two-dimensional model is formulated in a finite element, with the C0 element consisting of seven nodal unknowns per node. The final material properties of FG-CNT-reinforced rhombic laminates are estimated using the rule of mixture. The obtained numerical are compared with the results available in the literature to verify the reliability of the present model. The present study investigates the effect of CNT distribution, loading pattern, volume fraction, and various combinations of boundary constraints by developing a finite element code in FORTRAN.carbon nanotubesstructureskewfinite element methoddeflectionfrequency, A 003 Vol. 8 działalność statutowa WNET PSW CC-BY 2076-3417003Static and Dynamic Response of FG-CNT-Reinforced Rhombic LaminatesApplied Sciences20182076-34172017/201810.3390/app8050834Andrzejuk, WojciechplatesFINAL_PUBLISHEDThe present study focuses on the static and dynamic response of functionally graded carbon nanotube (FG-CNT)-reinforced rhombic laminates. The cubic variation of thickness coordinate in the displacement field is considered in terms of Taylor's series expansion, which represents the higher-order transverse cross-sectional deformation modes. The condition of zero-transverse shear strain at upper and lower surface of FG-CNT-reinforced rhombic laminates is imposed in the present formulation. The present two-dimensional model is formulated in a finite element, with the C0 element consisting of seven nodal unknowns per node. The final material properties of FG-CNT-reinforced rhombic laminates are estimated using the rule of mixture. The obtained numerical are compared with the results available in the literature to verify the reliability of the present model. The present study investigates the effect of CNT distribution, loading pattern, volume fraction, and various combinations of boundary constraints by developing a finite element code in FORTRAN.carbon nanotubesstructureskewfinite element methoddeflectionfrequency.
Tytuł pracy:
Charakterystyka formalna: ansverse cross-sectional deformation modes. The condition of zero-transverse shear strain at upper and lower surface of FG-CNT-reinforced rhombic laminates is imposed in the present formulation. The present two-dimensional model is formulated in a finite element, with the C0 element consisting of seven nodal unknowns per node. The final material properties of FG-CNT-reinforced rhombic laminates are estimated using the rule of mixture. The obtained numerical are compared with the results available in the literature to verify the reliability of the present model. The present study investigates the effect of CNT distribution, loading pattern, volume fraction, and various combinations of boundary constraints by developing a finite element code in FORTRAN.^acarbon nanotubes^astructure^askew^afinite element method^adeflection^afrequency
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