NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
An Immersed Boundary Method for Solving the Compressible Navier-Stokes Equations with Fluid Structure InteractionAn immersed boundary method for the compressible Navier-Stokes equation and the additional infrastructure that is needed to solve moving boundary problems and fully coupled fluid-structure interaction is described. All the methods described in this paper were implemented in NASA's LAVA solver framework. The underlying immersed boundary method is based on the locally stabilized immersed boundary method that was previously introduced by the authors. In the present paper this method is extended to account for all aspects that are involved for fluid structure interaction simulations, such as fast geometry queries and stencil computations, the treatment of freshly cleared cells, and the coupling of the computational fluid dynamics solver with a linear structural finite element method. The current approach is validated for moving boundary problems with prescribed body motion and fully coupled fluid structure interaction problems in 2D and 3D. As part of the validation procedure, results from the second AIAA aeroelastic prediction workshop are also presented. The current paper is regarded as a proof of concept study, while more advanced methods for fluid structure interaction are currently being investigated, such as geometric and material nonlinearities, and advanced coupling approaches.
Document ID
20170000312
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Brehm, Christoph
(Science and Technology Corp. Moffett Field, CA, United States)
Barad, Michael F.
(NASA Ames Research Center Moffett Field, CA United States)
Kiris, Cetin C.
(NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
January 11, 2017
Publication Date
June 12, 2016
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
ARC-E-DAA-TN32637
Report Number: ARC-E-DAA-TN32637
Meeting Information
Meeting: AIAA AVIATION 2016
Location: Washington, DC
Country: United States
Start Date: June 13, 2016
End Date: June 17, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNX15AW29G
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Equations
Immersed
Boundary
No Preview Available