1993
DOI: 10.1016/0045-7949(93)90378-q
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Dynamic analysis of laminates with elliptical cutouts using the hybrid-stress finite element

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Cited by 11 publications
(4 citation statements)
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“…Three different types of orthotropic materials namely (1) Carbon/Epoxy, (2) Kevlar49/Epoxy and (3) E-Glass/Epoxy are used for the analysis. These three material properties Ramakrishna [3] and Isaac [9] are provided in Table II.…”
Section: Ematerials Propertiesmentioning
confidence: 99%
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“…Three different types of orthotropic materials namely (1) Carbon/Epoxy, (2) Kevlar49/Epoxy and (3) E-Glass/Epoxy are used for the analysis. These three material properties Ramakrishna [3] and Isaac [9] are provided in Table II.…”
Section: Ematerials Propertiesmentioning
confidence: 99%
“…The different arrangements of hybrid laminates considered are 1/2/1/2, 1/2/2/1, 2/1/2/1, 2/1/1/2, 1/3/1/3, 1/3/3/1, 3/1/3/1, 3/1/1/3. The first material laminate is taken as carbon/epoxy (1), the second material laminate is taken as kevlar49/epoxy (2) and the third material laminate is taken as E-Glass/ Epoxy (3). For this hybrid laminate arrangements, the different lamination schemes are taken 0/0/0/0, 0/90/90/0 and 90/90/90/90.…”
Section: Influence Of Hybrid Arrangement In Specially Orthotropicmentioning
confidence: 99%
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“…Bicos and Springer [16,17] applied Reddy's higher order theory [15] and "nite element methods for the free damped and undamped vibration of laminated composite plates and shells with a concentric circular hole. Ramkrishna et al [18] used an eight-noded hybrid-stress isoparametric "nite element for the free vibration analysis of simply supported laminates with a concentric elliptical hole. Young et al [19] presented a Rayleigh}Ritz approach using the three-dimensional elasticity theory for the analysis of the free vibration of isotropic, thick, rectangular plates, with depressions, grooves, or cutouts.…”
Section: Introductionmentioning
confidence: 99%