Bonnie Jonkman

Results 10 issues of Bonnie Jonkman

This PR can be merged after #1042. **Feature or improvement description** This pull request primarily cleans up some of the AeroDyn code (and its submodules) to better sync with the...

Type: Bug
Module: AeroDyn

**Feature or improvement description** This PR merges more parts of the `TwrInfl` and `TwrInflArray`, which are basically two copies of the tower influence calculations, one for the BEMT module and...

Module: AeroDyn
Approved: Update baselines

**Feature or improvement description** The check to turn off BEM for low TSRs should have been using `ABS(TSR)` instead of `TSR` so that BEM is not disabled for all negative...

Module: AeroDyn
Approved: Update baselines

In looking through the AeroAcoustics module documentation, I noticed sub-sections of the primary AeroDyn input file (and airfoil files) were duplicated there. The sections referenced in the AA documentation had...

Type: Enhancement

**Bug description** When NLinTimes > 1 and CalcSteady = true, OpenFAST will wait for steady state to begin linearization. However, when NLinTimes = 1 (and RotSpeed is non-zero), the first...

Type: Bug

#1217 changed the r-test suite, but there are a few things it missed: - [x] The `manualRegressionTest.py` script should be changed so that it works with the updated `execute*RegressionCase.py` files....

Type: Bug
Type: Testing
Type: Documentation

The Visual Studio project files that contain NWTC_Library need to be updated with the new names of the Registry input files in the `dev-unstable-pointers` branch. They currently reference `..\..\modules\nwtc-library\src\Registry_NWTC_Library_typedef_nomesh.txt` and...

System: Visual Studio

When running the OpenFAST `Tailfin_FreeYaw1DOF_PolarBased` case, this warning appears: > FAST_InitializeAll:AD_Init:Init_AFIparams:AFI_Init:ReadAFfile:Airfoil data should go from -180 > degrees to 180 degrees and the coefficients at the ends should be the...

**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...

Module: AeroDyn

While debugging some differences in a new method of calculating default unsteady airfoil coefficients, I noticed some unusual characteristics in the lift coefficients in several of the aerodyn/BAR_Baseline files (1-6)....