Extends OpenAeroStruct critical section method to enable different airfoil maximum lift coefficients across the span. This enables modeling of high lift devices that do not extend across the entire span.
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Bugfix (non-breaking change which fixes an issue)
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Purpose
Extends OpenAeroStruct critical section method to enable different airfoil maximum lift coefficients across the span. This enables modeling of high lift devices that do not extend across the entire span.
Type of change
What types of change is it? Select the appropriate type(s) that describe this PR
Testing
Explain the steps needed to test the new code to verify that it does indeed address the issue and produce the expected behavior.
Checklist
Put an
xin the boxes that apply.