MIT Libraries logoDSpace@MIT

MIT
View Item 
  • DSpace@MIT Home
  • Department of Aeronautics and Astronautics
  • Aerospace Computational Design Laboratory
  • Aerospace Computational Design Laboratory: Technical Reports
  • View Item
  • DSpace@MIT Home
  • Department of Aeronautics and Astronautics
  • Aerospace Computational Design Laboratory
  • Aerospace Computational Design Laboratory: Technical Reports
  • View Item
JavaScript is disabled for your browser. Some features of this site may not work without it.

Solution of Fluid-Structure Interaction Problems using a Discontinuous Galerkin Technique

Author(s)
Mohnot, Anshul
Thumbnail
DownloadACDL_TR-08-4.pdf (1.922Mb)
Metadata
Show full item record
Abstract
The present work aims to address the problem of fluid-structure interaction using a discontinuous Galerkin approach. Starting from the Navier-Stokes equations on a fixed domain, an arbitrary Lagrangian Eulerian (ALE) approach is used to derive the equations for the deforming domain. A geometric conservation law (GCL) is then introduced, which guarantees freestream preservation of the numerical scheme. The space discretization is performed using a discontinuous Galerkin method and time integration is performed using either an explicit four stage Runge-Kutta scheme or an implicit BDF2 scheme. The mapping parameters for the ALE formulation are then obtained using algorithms based on radial basis functions (RBF) or linear elasticity. These strategies are robust and can be applied to bodies with arbitrary shapes and undergoing arbitrary motions. The robustnesss and accuracy of the ALE scheme coupled with these mapping strategies is then demonstrated by solving some model problems. The ability of the scheme to handle complex flow problems is demonstrated by analyzing the low Reynolds number flow over an oscillating circular cylinder.
Date issued
2008-05
URI
http://hdl.handle.net/1721.1/57609
Publisher
Aerospace Computational Design Laboratory, Dept. of Aeronautics & Astronautics, Massachusetts Institute of Technology
Series/Report no.
ACDL Technical Reports;ACDL TR-08-4

Collections
  • Aerospace Computational Design Laboratory: Technical Reports

Browse

All of DSpaceCommunities & CollectionsBy Issue DateAuthorsTitlesSubjectsThis CollectionBy Issue DateAuthorsTitlesSubjects

My Account

Login

Statistics

OA StatisticsStatistics by CountryStatistics by Department
MIT Libraries
PrivacyPermissionsAccessibilityContact us
MIT
Content created by the MIT Libraries, CC BY-NC unless otherwise noted. Notify us about copyright concerns.