Tapered composite beams formed by terminating or dropping-off some of the plies from primary structure are being used in various engineering applications. Because of their structural tailoring capabilities, damage tolerance and potential for creating significant weight savings in helicopter yoke, robot arms and turbine blades, tapered composite beams have received much attention from engineers and researchers. Design of mechanical components using tapered composite beams requires a better understanding of their behavior on free and forced vibrations.Free and forced vibration analysis including the effects of axial force and damping of tapered composite beams is conducted using conventional, and higher-order finite elements and the Rayleigh-Ritz method. Composite beam samples are manufactured and tested for the determination of mechanical properties and damping loss factor.A detailed parametric study is conducted to investigate the effects of boundary conditions, laminate configuration, taper configurations, taper angle, the ratio of the length of the thick section to the length of thin section, axial force, and damping.
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HASNET EFTAKHER UDDIN AHMED FINISHED HIS BS'c IN MECHANICAL ENGINEERING FROM BANGLADESH UNIVERSITY OF ENGINEERING AND TECHNOLOGY (BUET).THEN HE CAME TO CONCORDIA UNIVERSITY, MONTREAL,CANADA FOR HIS MASTER'S OF APPLIED SCIENCE IN MECHANICAL ENGINEERING WHERE HE DID THIS WORK. NOW HE IS CONTINUING HIS PHD IN U OF T, CANADA.
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Taschenbuch. Etat : Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Tapered composite beams formed by terminating or dropping-off some of the plies from primary structure are being used in various engineering applications. Because of their structural tailoring capabilities, damage tolerance and potential for creating significant weight savings in helicopter yoke, robot arms and turbine blades, tapered composite beams have received much attention from engineers and researchers. Design of mechanical components using tapered composite beams requires a better understanding of their behavior on free and forced vibrations.Free and forced vibration analysis including the effects of axial force and damping of tapered composite beams is conducted using conventional, and higher-order finite elements and the Rayleigh-Ritz method. Composite beam samples are manufactured and tested for the determination of mechanical properties and damping loss factor.A detailed parametric study is conducted to investigate the effects of boundary conditions, laminate configuration, taper configurations, taper angle, the ratio of the length of the thick section to the length of thin section, axial force, and damping. 300 pp. Englisch. N° de réf. du vendeur 9783838313306
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Etat : New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Tapered composite beams formed by terminating or dropping-off some of the plies from primary structure are being used in various engineering applications. Because of their structural tailoring capabilities, damage tolerance and potential for creating signif. N° de réf. du vendeur 5412025
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Taschenbuch. Etat : Neu. Vibration Analysis of Tapered Composite Materials | Experiment and Finite element analysis | Hasnet Ahmed | Taschenbuch | 300 S. | Englisch | 2009 | LAP LAMBERT Academic Publishing | EAN 9783838313306 | Verantwortliche Person für die EU: BoD - Books on Demand, In de Tarpen 42, 22848 Norderstedt, info[at]bod[dot]de | Anbieter: preigu. N° de réf. du vendeur 101490306
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Taschenbuch. Etat : Neu. This item is printed on demand - Print on Demand Titel. Neuware -Tapered composite beams formed by terminating or dropping-off some of the plies from primary structure are being used in various engineering applications. Because of their structural tailoring capabilities, damage tolerance and potential for creating significant weight savings in helicopter yoke, robot arms and turbine blades, tapered composite beams have received much attention from engineers and researchers. Design of mechanical components using tapered composite beams requires a better understanding of their behavior on free and forced vibrations.Free and forced vibration analysis including the effects of axial force and damping of tapered composite beams is conducted using conventional, and higher-order finite elements and the Rayleigh-Ritz method. Composite beam samples are manufactured and tested for the determination of mechanical properties and damping loss factor.A detailed parametric study is conducted to investigate the effects of boundary conditions, laminate configuration, taper configurations, taper angle, the ratio of the length of the thick section to the length of thin section, axial force, and damping.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 300 pp. Englisch. N° de réf. du vendeur 9783838313306
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Taschenbuch. Etat : Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Tapered composite beams formed by terminating or dropping-off some of the plies from primary structure are being used in various engineering applications. Because of their structural tailoring capabilities, damage tolerance and potential for creating significant weight savings in helicopter yoke, robot arms and turbine blades, tapered composite beams have received much attention from engineers and researchers. Design of mechanical components using tapered composite beams requires a better understanding of their behavior on free and forced vibrations.Free and forced vibration analysis including the effects of axial force and damping of tapered composite beams is conducted using conventional, and higher-order finite elements and the Rayleigh-Ritz method. Composite beam samples are manufactured and tested for the determination of mechanical properties and damping loss factor.A detailed parametric study is conducted to investigate the effects of boundary conditions, laminate configuration, taper configurations, taper angle, the ratio of the length of the thick section to the length of thin section, axial force, and damping. N° de réf. du vendeur 9783838313306
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