From 5a5290dbd47db45638bb7efb1228fefed686e7fa Mon Sep 17 00:00:00 2001 From: Mayank Chetan Date: Tue, 2 Aug 2022 11:52:51 -0600 Subject: [PATCH] typo in AeroDyn input file comments --- weis/aeroelasticse/FAST_writer.py | 4 ++-- 1 file changed, 2 insertions(+), 2 deletions(-) diff --git a/weis/aeroelasticse/FAST_writer.py b/weis/aeroelasticse/FAST_writer.py index 8e441f237..5dedc2e06 100644 --- a/weis/aeroelasticse/FAST_writer.py +++ b/weis/aeroelasticse/FAST_writer.py @@ -738,7 +738,7 @@ def write_AeroDyn15(self): f.write('{:<22} {:<11} {:}'.format(self.fst_vt['AeroDyn15']['SpdSound'], 'SpdSound', '- Speed of sound (m/s)\n')) f.write('{:<22} {:<11} {:}'.format(self.fst_vt['AeroDyn15']['Patm'], 'Patm', '- Atmospheric pressure (Pa) [used only when CavitCheck=True]\n')) f.write('{:<22} {:<11} {:}'.format(self.fst_vt['AeroDyn15']['Pvap'], 'Pvap', '- Vapour pressure of fluid (Pa) [used only when CavitCheck=True]\n')) - f.write('====== Blade-Element/Momentum Theory Options ====================================================== [used only when WakeMod=1]\n') + f.write('====== Blade-Element/Momentum Theory Options ====================================================== [unused when WakeMod=0 or 3]\n') f.write('{:<22d} {:<11} {:}'.format(self.fst_vt['AeroDyn15']['SkewMod'], 'SkewMod', '- Type of skewed-wake correction model (switch) {1=uncoupled, 2=Pitt/Peters, 3=coupled} [unused when WakeMod=0 or 3]\n')) f.write('{!s:<22} {:<11} {:}'.format(self.fst_vt['AeroDyn15']['SkewModFactor'], 'SkewModFactor', '- Constant used in Pitt/Peters skewed wake model {or "default" is 15/32*pi} (-) [used only when SkewMod=2; unused when WakeMod=0 or 3]\n')) f.write('{!s:<22} {:<11} {:}'.format(self.fst_vt['AeroDyn15']['TipLoss'], 'TipLoss', '- Use the Prandtl tip-loss model? (flag) [unused when WakeMod=0 or 3]\n')) @@ -748,7 +748,7 @@ def write_AeroDyn15(self): f.write('{!s:<22} {:<11} {:}'.format(self.fst_vt['AeroDyn15']['TIDrag'], 'TIDrag', '- Include the drag term in the tangential-induction calculation? (flag) [unused when WakeMod=0,3 or TanInd=FALSE]\n')) f.write('{:<22} {:<11} {:}'.format(self.fst_vt['AeroDyn15']['IndToler'], 'IndToler', '- Convergence tolerance for BEMT nonlinear solve residual equation {or "default"} (-) [unused when WakeMod=0 or 3]\n')) f.write('{:<22d} {:<11} {:}'.format(self.fst_vt['AeroDyn15']['MaxIter'], 'MaxIter', '- Maximum number of iteration steps (-) [unused when WakeMod=0]\n')) - f.write('====== Dynamic Blade-Element/Momentum Theory Options ====================================================== [used only when WakeMod=1]\n') + f.write('====== Dynamic Blade-Element/Momentum Theory Options ====================================================== [used only when WakeMod=2]\n') f.write('{:<22d} {:<11} {:}'.format(self.fst_vt['AeroDyn15']['DBEMT_Mod'], 'DBEMT_Mod', '- Type of dynamic BEMT (DBEMT) model {1=constant tau1, 2=time-dependent tau1} (-) [used only when WakeMod=2]\n')) f.write('{:<22} {:<11} {:}'.format(self.fst_vt['AeroDyn15']['tau1_const'], 'tau1_const', '- Time constant for DBEMT (s) [used only when WakeMod=2 and DBEMT_Mod=1]\n')) f.write('====== OLAF -- cOnvecting LAgrangian Filaments (Free Vortex Wake) Theory Options ================== [used only when WakeMod=3]\n')