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SC/Tetra
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SC/Tetra
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HEAT Designer
CADthru
In addition to solving basic fluid flow and heat transfer problems, SC/Tetra is equipped with many physical models capable of simulating a wide variety of industrial applications.
ALE (Moving and/or Rotating Boundaries) / Overset mesh / Dynamic ALE
SC/Tetra is equipped with ALE (moving and/or rotating boundaries) which enables  simulating airflow caused by a moving object.  This can include rotating fan blades or cars passing by one another.

SC/Tetra Version 7 is also equipped with an overset mesh function which allows different sets of meshes to overlap. This enables an object to move freely without having to generate and eliminate mesh which is usually a very complicated process.


In addition, the dynamic ALE function enables an object to translate or rotate in response to a force caused by surrounding airflow.
Human Body Thermoregulatory Model (JOS)
JThe OS Thermoregulatory Model is developed by Prof. Tanabe at Waseda University.  JOS calculates the human body skin surface temperature by considering energy transportation using a detailed vascular system model and physiological characterization of the human body. At the same time, JOS also considers heat and moisture generated from the human body and reflected  to the surrounding environment.
Electric Current (Joule Heating) Analysis
Joule heat generated by an electric potential can be predicted and used as the boundary condition for an electrical heating wire.  By specifying the electric potential at each end of the wire, electric current density, and electrical. conductivity, the electric potential field and heat flux at an location can be predicted.
Cavitation
The cavitation  function predicts cavitation due to pressure changes in the fluid. While SC/Tetra does not generate vapor due to cavitation it can predict where cavitation may occur.
Aeroacoustic Analysis
SC/Tetra is equipped with the following three acoustic analytical functions:

1) Decomposition of a flow and associated acoustic fields and use of the acoustic
analogy method for noise prediction at a far field observing point away from the noise source,

2) Weak compressible flow model for resonant sound, and

3) Sound source detection method for detecting a sound source.
Aeroacoustic Analysis is usually calculated using LES (Large Eddy Simulation). However, sound source detection analysis can be calculated using the k-ε turbulence model and steady state analysis.

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