Numerical Approximation of Fluid Structure Interaction (FSI) Problem | Simplified Model for the Vertical Vibrations of the Aircraft Wing

Bhuiyan Shameem Mahmood Ebna Hai

ISBN 10: 3659302848 / ISBN 13: 9783659302848

Published by LAP Lambert Academic Publishing, 2012

About this Item

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: LAP Lambert Academic Publishing, Brivibas Gatve 197, 1039 RIGA, LETTLAND, customerservice[at]vdm-vsg[dot]de | Anbieter: preigu.

Seller Inventory # 106165003

Bibliographic Details

• Title: Numerical Approximation of Fluid Structure Interaction (FSI) Problem | Simplified Model for the Vertical Vibrations of the Aircraft Wing
• Publisher: LAP Lambert Academic Publishing
• Publication Date: 2012
• Language: English
• ISBN 10: 3659302848
• ISBN 13: 9783659302848
• Binding: Taschenbuch
• Condition: Neu
• Dimensions: 6W x 150H x 220D millimeters 6 millimeters width by 150 millimeters height by 220 millimeters depth
• Weight: 135 grams
• Seller catalogs:
  • Bücher

About this title

Synopsis

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.

About the Author

Mr. 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 University of Hamburg. His research interests include Numerical Simulation Techniques and Fluid Dynamics. He published several articles in refereed journals.