Yaml Input File Update

[kevmoor]

Updates to unify the file input option for standard turbine types (e.g. fixed bottom Darrius and H-VAWT with arbitrary blade shapes and numbers of struts), improve/add documentation for this run method.

[codecov]

Codecov Report

Attention: Patch coverage is 19.23848% with 403 lines in your changes missing coverage. Please review.

Project coverage is 41.48%. Comparing base (f95124d) to head (ba63fdd).
Report is 26 commits behind head on master.

Files with missing lines	Patch %	Lines
src/windio.jl	0.00%	199 Missing ⚠️
src/topRunDLC.jl	0.00%	146 Missing ⚠️
src/fileio.jl	64.19%	29 Missing ⚠️
src/SetupTurbine.jl	20.00%	12 Missing ⚠️
src/Unsteady.jl	69.23%	8 Missing ⚠️
src/utilities.jl	72.22%	5 Missing ⚠️
src/Unsteady_Land.jl	71.42%	2 Missing ⚠️
src/gxbeam_conversion.jl	0.00%	2 Missing ⚠️

Additional details and impacted files

@@            Coverage Diff             @@
##           master      #91      +/-   ##
==========================================
- Coverage   41.87%   41.48%   -0.39%     
==========================================
  Files          15       15              
  Lines        6085     6147      +62     
==========================================
+ Hits         2548     2550       +2     
- Misses       3537     3597      +60     

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[kevmoor]

Windio Changes:

• Gravity single value or array of 3, is in the global frame of reference, so positive gravity would be pulling the structure up.
• Start and end nd_arc values are the only input supported. Otherwise, there are as many as 12 different ways to specify this input.
• Grids must be defined from end to end, set number of plies to 1e-6 at unused spanwise sections.
• The blade object is reused for the tower, struts, cables, etc. since these elements can be modeled at the same fidelity as the blade and can be simplified via simpler inputs, but the other definitions don't allow for simpler inputs.
• Rotor_orientation for VAWTs is determined by the gravity vector, so the rest of the coordinate systems are the same at this time, plans include multiple arbitrary rotation axes for different portions of the structure.
• Material A is stress amplitude, and m is cycles to failure in log10, i.e. 10^6, 10^20.
  A: [420.0,415.0,375.0,275.0,190.0,0.0]
  m: [0.0,1.0,2.0,4.0,6.0,20.0]

Variable Name Changes:

• outFilename to dataOutputFilename
• AModel to AeroModel
• DSModel to DynamicStallModel
• saveName to VTKsaveName
• hydroOn to platformActive
• turbsimpath to turbsimsavepath
• numDofPerNode to numDOFPerNode