anne/tasmet
1
0
Fork 0
Code Issues Pull Requests Releases Wiki Activity
Thermoacoustic System Modeling Environment Twente
21 Commits 1 Branch 0 Tags 5.4 MiB
C++ 87.6%
Python 9.2%
CMake 2.4%
C 0.8%
c4ffca4640
Go to file
J.A. de Jong @ vulgaris c4ffca4640 Updated added adiabaticwall and doxyfile.
2017-01-05 15:33:13 +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 added adiabaticwall and doxyfile. 2017-01-05 15:33:13 +01:00
testing Whole lotta further 2016-12-15 21:34:11 +01:00
.gitattributes Added documentation as-is 2016-11-11 23:25:44 +01:00
.gitignore Continue... 2016-12-29 19:06:16 +01:00
CMakeLists.txt Updated added adiabaticwall and doxyfile. 2017-01-05 15:33:13 +01:00
Doxyfile Updated added adiabaticwall and doxyfile. 2017-01-05 15:33:13 +01:00
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