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Ran 28 Apr 2017 01:28AM UTC

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Committed 28 Apr 2017 01:25AM UTC coverage: 70.491% (-0.8%) from 71.321%

Job # FORTRAN=1 PY=2.7

Build Type

push

travis-ci

Committed by

web-flow

Commit Message

Added trim constraint (#25)

* Nonfunctional; start of trim calculations; Fortran segfaulting

* Nonfunctional; debugging structural deriv

* CM constraint working; derivatives included

* Slight clean-up

* Renamed 'stress' to 'yield' and updated plot_all to use the saved yield value

* Only use Aitken if it's installed

* Updated CM to calculate moments with forces acting at mid bound points

* Added naive static margin computation for after a run

* Updated initial radii function to correctly use the radius instead of the diamater value for the given mesh. This effectively makes the initial tube half the radius of before.

* Changed CM calculation to be in a total_performance group

* Changed cg and CM to be updated with structural weight

* Small updates to make tests pass

* Moved assembleK outside the coupled loop

* Temporarily modified for MDO assignment

* Removing some modifications from the assignment

* Adding comment throughout. Readded option to use weighted objective function for aerostructural optimization

* Added slight comments

* Updated comments throughout

* Updated comments and UAV problem

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