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Add coordinate derivatives for aero and structural disciplines to the MeldThermal class
Should just involve differentiating the weight matrix involved in the T and Q residuals w.r.t. xa0 and xs0
Will have to add to MeldThermal.cpp, TransferScheme.pxd, TransferScheme.pyx, and the body.py file
Discovered these features are missing because the aerothermal coordinate derivatives in my coordinate derivatives unittest for the TacsOnewayDriver were off by 100%. Aerothermoelastic was very off too
The text was updated successfully, but these errors were encountered:
Apparently we didn't use to need them. However, now with number of aero nodes and struct nodes changing the weight matrix for thermal transfer will change when integrated with ESP/CAPS shape optimization. Therefore we need these coordinate derivatives now
We fix the aerodynamic + structural coordinates for the thermal transfer scheme. This may cause remeshing shape derivatives to be less accurate. However, that is why we need structural mesh morphing. Closing this issue for now
xa0
andxs0
TacsOnewayDriver
were off by 100%. Aerothermoelastic was very off tooThe text was updated successfully, but these errors were encountered: