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mdolab / OpenAeroStruct / 40
97%

Build:
DEFAULT BRANCH: master
Ran 15 Apr 2017 03:36PM UTC
Jobs 3
Files 10
Run time 2min
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Add clarity to some variables, changed default yield stress, updated docs (#22)

* Fixed failing tests

* Changed 'weight' to 'structural_weight' and added clarity in docs and comments

* Added aerostructural tutorial

* Changed default value of yield stress to be more realistic for aircraft aluminum. Added option for user to input displacements

* Slight changes to get analysis.py working with the new variable names

* Updated HW tips and fixed bug where inputted thickness was not accessed correctly.

2084 of 2514 relevant lines covered (82.9%)

1.36 hits per line

Jobs
ID Job ID Ran Files Coverage
1 40.1 (FORTRAN= PY=2.7) 15 Apr 2017 03:36PM UTC 0
64.6
Travis Job 40.1
2 40.2 (FORTRAN= PY=3.4) 15 Apr 2017 03:36PM UTC 0
0.04
Travis Job 40.2
3 40.3 (FORTRAN=1 PY=2.7) 15 Apr 2017 03:38PM UTC 0
71.32
Travis Job 40.3
Source Files on build 40
Detailed source file information is not available for this build.
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