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v1.3.2

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@lucas-carmo lucas-carmo released this 10 Jan 19:39
0bcc3ae

Overview

This release includes bug fixes only:

  • Bug fixes in member.getInertia() and cap info for rectangular members (097c264). In particular, fixed a bug when reading cap_d_in from the yaml file for rectangular elements (previous code to read cap_d_in worked for circular cylinders only).
  • Bug fix of the rotor moments from CCBlade. 'Q' output from CCBlade was in the 'pitch' spot and 'My' output from CCBlade was in the 'roll' spot - they were flipped and now things are correct. Also updated the default vapor pressure when calculating cavitation (cf839a8)
  • Bug fix to account for rotor orientation in model.solveStatis(). The rotor orientation is set internally depending on yaw_mode, but this was done only after computing the inertial properties of the system in solveStatics(). Consequently, the weight of the RNA was acting as if the turbine was at its initial position regardless of yaw_mode. Now, rotor orientation is updated before computing the inertial properties of the system. (b5d2591 and 69b8695)
  • Included tests for QTFs computed with RAFT and for the MacCamy-Fuchs correction (173c8be)
  • We were missing a term from Rainey's formulation in the computation of RAFT QTFs (7835e39)
  • The total mass and the x coordinate of the center of gravity of the RNA of the IEA15 MW turbine were wrong in examples/VolturnUS-S_example.yaml, tests/test_data/IEA15MW.yaml, tests/test_data/VolturnUS-S.yaml and tests/test_data/VolturnUS-S_farm.yaml (cb14509)
  • Flag aeroServoMod was misspelled in some input files (f69e88b)

Changes that do not affect users or previous results:

What's Changed

Full Changelog: v1.3.1...v1.3.2