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mdolab / OpenAeroStruct / 50 / 3
97%
master: 97%

Build:
DEFAULT BRANCH: master
Ran 06 May 2017 04:13AM UTC
Files 11
Run time 0s
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06 May 2017 04:09AM UTC coverage: 71.107% (+0.7%) from 70.448%
FORTRAN=1 PY=2.7

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User can now input reference area for coefficient calculations (#27)

* Added small comments to plot_all

* Fixed bug in intersecting thickness constraint

* Updated fem_origin in plot_all so it uses the actual value from the problem

* Reworked CM calculation

* User can now set an aircraft reference area. Updated moment, fuelburn, and total CL/CD calculations.

* Fixed CM derivatives

2023 of 2845 relevant lines covered (71.11%)

0.71 hits per line

Source Files on job 50.3 (FORTRAN=1 PY=2.7)
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Coverage ∆ File Lines Relevant Covered Missed Hits/Line
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