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Thermoacoustic System Modeling Environment Twente
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Anne de Jong e255b9e2c9 Updated all GUI stuff to new protobuf config of model containing a system, solver and solution
2017-01-05 16:25:16 +01:00
doc Tested 1D-solver, added adiabatictemp, which solves the adiabatic temperature change due to a pressure change 2016-12-02 22:47:07 +01:00
src Updated all GUI stuff to new protobuf config of model containing a system, solver and solution 2017-01-05 16:25:16 +01:00
testing Whole lotta further 2016-12-15 21:34:11 +01:00
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CMakeLists.txt Updated added adiabaticwall and doxyfile. 2017-01-05 15:33:13 +01:00
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README.md Added documentation as-is 2016-11-11 23:25:44 +01:00

README.md

TaSMET

Thermoacoustic System Modeling Environment Twente

Welcome to the ThermoAcoustic System Modeling Environment Twente, or TASMET. TASMET is a computer code to model thermoacoustic (TA) engines, refrigerators and combined systems by providing nonlinear models for laminar/turbulent oscillating flow in ducts, heat exchangers and stacks/regenerators. A coupling to the mechanical and electrical domain is provided with a piston model.

  • For a quick glance on the possibilities of TaSMET, please look into the User's guide provided with the code.
  • For the installation guide, please look into the Wiki
  • Examples of working models will be provided. We are currently working on that. Once a regenerator model is implemented, we will provide examples of Stirling models.

Example models

Example models for TaSMET will be provided in the tasmet_examples repository.

Release notes version 0.1

  • Stacks cannot yet be connected to ConnectorVolumes
  • Stacks cannot yet be connected to Pistons
  • VelocityBc probably still has a bug