This content describes enhancements to the thermal output type of a co-simulation interface's simulation object in some center 3D. Users can now select different sources of heat flux to exchange with external solvers, including convective radiative thermal loads or orbital heat flux sources computed on a specific part of the model. This allows for accurate evaluation of the battery state of charge for a spacecraft during a specific orbit mission.
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Негізгі бет Simcenter 3D 2406 Thermal Multiphysics Co-Simulation to Systems Simulation
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