Fluid-Structure Interaction: EDGE
[2007-?]
An interface between MBDyn and EDGE, a Navier-Stokes solver for unstructured grids developed by FOI (Swedish Defense Research Agency), is being developed.
News
- 2010-10-01: Luca is back to Politecnico di Milano as senior researcher. Congratulations, and good luck!
- 2009-05-01: Luca now works at FOI. Good luck!
- 2009-04-01: L. Cavagna, P. Masarati, and G. Quaranta: “Simulation of Maneuvering Flexible Aircraft by Coupled Multibody/CFD” presented at the ECCOMAS Thematic Conference on Multibody Dynamics, June 29-July 2, 2009, Warsaw University of Technology, Warsaw, Poland.
- 2008-11-06: This presentation: L. Cavagna, P. Masarati, G. Quaranta, M. Mantegazza “Application of Fluid-Structure Tight Interaction by Multibody/CFD Simulation to Aircraft Aeroelasticity in Free Flight” was given at the SAAB Flygtekniskt Seminar 2008, November 5-6, 2008, Kolmården, Sweden.
- 2008-10-20: Interface with MBDyn’s rigid- & modal-body is there :) See the external forces section of the input manual.
- 2008-04-12: Maneuver capabilities added to EDGE.
- 2008-02-01: Luca is back.
- 2008-01-17: The radial basis functions interface for FSI with EDGE is now fully implemented.
- 2007-12-28: The interface to an external program for generalized component mode synthesis coupling is now implemented in MBDyn.
- 2007-12-13: The moving least-square interface for FSI with EDGE is now fully implemented.
- 2007-11-15: presentation at FOI.
- 2007-11-06: EDGE now fully supports the computation of the classical unsteady aerodynamics matrix Ham(p) in the reduced frequency-domain p, based on given structure motion shapes.
- 2007-10-17: fixed transpiration for aeroelasticity without grid deformation when structural displacements are small.
- 2007-10-12: presentation of activity at FOI.
- 2007-09-28: Luca left.
Related links
- the TURNS interface research page
- the FreeCASE: Free(dom) Computational AeroServoElasticity project