Numerical Approximation Fluid Structure by Ebna Bhuiyan (4 results)
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Taschenbuch. Condition: Neu. Numerical Approximation of Fluid Structure Interaction (FSI) Problem | Simplified Model for the Vertical Vibrations of the Aircraft Wing | Bhuiyan Shameem Mahmood Ebna Hai | Taschenbuch | Englisch | LAP Lambert Academic Publishing | EAN 9783659302848 | Verantwortliche Person für die EU: preigu GmbH &… Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu.
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Paperback. Condition: Like New. LIKE NEW. SHIPS FROM MULTIPLE LOCATIONS. book.
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Seller: moluna, Greven, Germanymoluna
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Kartoniert / Broschiert. Condition: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Ebna Hai Bhuiyan Shameem MahmoodMr. Ebna Hai has received B.Sc degree in Mechanical Engineering from University of Dhaka [MIST], double M.Sc degree in Mathematical Modelling in…Engineering and in Industrial Mathematics from Universit.
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Seller: AHA-BUCH GmbH, Einbeck, GermanyAHA-BUCH GmbH
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Taschenbuch. Condition: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Now-a-days advanced composite materials are being applied to many aircraft structures in order to improve performance and save weight. But Aircraft wings can break due to FSI effect. Because of thrust force, turbulent flow, FSI plays an…important role and complex mechanical effects are aroused. But only numerical approaches can be used to solve such problems due to nonlinear properties of fluid, material and shape of the structures. The principal aim of this research is to explore and understand the behaviour of the FSI during the impact of a deformable material (of aircraft wings) on air. This project is focused on the analysis of Navier-Stokes and Elastodynamics equations in the ALE frameworks in order to simulate numerically the FSI effect on a double wedge airfoil. Also one of the main aims of this research is to study the Euler-Bernoulli Beam, the static and dynamic response of a cantilever beam, for a simplified model to determine the vertical vibration of the aircraft wings. In this case we use Approximate method in order to determine the vertical vibration and finally we choose a suitable space-dependent function that satisfy the requirements at the boundaries.
