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cuspaceflight / bamboo

Cooling system modelling for liquid rocket engines.
GNU Affero General Public License v3.0
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Geometry bug with small area combustion chambers #3

Closed dug20 closed 3 years ago

dug20 commented 3 years ago

There is a bug with the geometry of the converging section of the nozzle, if you use combustion chambers with too small an area.

(The fix should be relatively simple, but I just need to get around to it).

dug20 commented 3 years ago

Resolved