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Software
Computational Fluid Dynamics (CFD)
 


To support the task of improving the efficiency in turbomachinery CFD is applied to calculate the flow through thermal turbomachinery. The flow analysis shall help to reduce the losses inside the blade passages as well as in all flow guiding parts. For this purpose several self-developed and commercial CFD codes are in use.


  Codes in use:

  LINARS: HELP MENUE MAIN PAGE
   
Developed at the Institute for Thermal Turbomachinery and Machine Dynamics. The code is written in the object orientated programming language C++ and hence its easy to maintain or to implement new objects, for e.q. new boundary conditions or turbulence models.

The main features of the code are:
  • structured grids in multiblock alignment
  • finite volume spatial high order upwind scheme
  • high order discretization in time
  • fully implicit treatment of the equation system (ADI) with multigrid techniques (FAS)
  • various eddy viscosity turbulence models
  • laminar-turbulent transition
  • nonreflecting boundary conditions
  • phase lagged boundary conditions for unequal blade counts in stage calculations


  •   AVBP
        Developed at European Center for Research and Advanced Training in Scientific Computation, CERFACS

      TRACE:
        Developed at the Institute of Propulsion Technology, DLR , Germany
    more information (english): click here
    more information (german): click here

      Roe2D and Roe3D:
       
    Predecesor of LINARS, developed at the Institute for Thermal Turbomachinery and Machine Dynamics. Fully implicit time-marching Navier-Stokes solver using a cell-centered finite-volume scheme. It is able to consider multi-block grids, moving grids and rotor-stator interaction.

      UCAS:
       
    Solver for Unsteady CAScade flows (code developed at the Institute for Thermal Turbomachinery and Machine Dynamics), Thin-layer Reynolds-averaged Navier-Stokes code using a third-order accurate, upwind-biased Osher scheme. The algebraic Baldwin-Lomax and the one-equation Baldwin-Barth turbulence model are implemented together with different models for laminar-turbulent transition. Moving and deforming grids for aeroelasticity investigations can be considered.

      SWIFT/FIRE by AVL (commercial software)
        more information (english): click here

      FLUENT (commercial software)
        more information: click here


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    eMail: TTM@TUGraz.at // Contact informations & Impressum // TUGonline // Graz University of Technology © 2005