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cuspaceflight
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bamboo
Cooling system modelling for liquid rocket engines.
GNU Affero General Public License v3.0
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0.2.1
#47
Closed
dug20
closed
2 years ago
dug20
commented
2 years ago
Added additional validation cases.
Coolant flow solver can now accommodate compressible coolants automatically.
Removed fin heat transfer for now, as it was producing spurious results.
Corrected mistakes with spiralling channel geometry.
Swapped to using the recovery temperature instead of static temperature for the exhaust gas temperature in thermal circuits.