Aero modifications

[bjonkman]

Feature or improvement description This pull request

• makes some modifications to UAMod 5 for use in full 360-degree angles of attack.
• uses a weighted-average of the axial induction for DBEMT input instead of just a uniform average of axial induction at all the nodes.
• allows the user to change the IntegrationMethod used in UA (UA_Mod 4, 5, etc)
• allows the user to have the code calculate CantAngle (if BlCrvAng is not specified in the input file). These calculated values are printed in the summary file.
• caps the Ct, Cp, and Cq outputs if their denominators ever get too small
• implemented the code around BldNd_BlOutNd in AeroDyn, allowing the user to specify which nodes they would like to output.
• fixes an issue where the AeroDyn echo file would not include blade property files.
• reports an error if one exists in the BEMT initialization of states (likely rare)
• updates some calculations of the UA parameters in AFI initialization
• removes non-standard tabs from MoorDyn
• changes TwrAero from a logical to integer internally (the input file still recognizes the logical value)
• simplifies some logic around the buoyancy calculations

Related issue, if one exists

Impacted areas of the software AeroDyn: DBEMT, UA (UA_Mod 4, 5, or 6)

Additional supporting information

Test results, if applicable

Failing cases:

• ad_BAR_SineMotion_UA4_DBEMT3

  • This has differences in the InflowWind output channel; I need to understand what would cause this this a little better before merging.
  • 
  • 

• MHK_RM1_Fixed

  • The differences here are minor:

• Fake5MW_AeroLin_B1_UA4_DBEMT3

  • Frequencies are less than 0.3% different (less than 0.009 Hz)
  • Damping is within 0.01%

• Fake5MW_AeroLin_B3_UA6

  • Frequencies are less than 0.2% different (less than 0.001 Hz)
  • Damping is within 0.005%