You signed in with another tab or window. Reload to refresh your session.You signed out in another tab or window. Reload to refresh your session.You switched accounts on another tab or window. Reload to refresh your session.Dismiss alert
{{ message }}
This repository was archived by the owner on Nov 27, 2023. It is now read-only.
1.464E-05 KinVisc - Kinematic air viscosity (m^2/s)
18
-
335 SpdSound - Speed of sound (m/s)
19
-
103500 Patm - Atmospheric pressure (Pa) [used only when CavitCheck=True]
20
-
1700 Pvap - Vapour pressure of fluid (Pa) [used only when CavitCheck=True]
21
-
0.5 FluidDepth - Water depth above mid-hub height (m) [used only when CavitCheck=True]
22
-
====== Blade-Element/Momentum Theory Options ====================================================== [unused when WakeMod=0 or 3]
23
-
2 SkewMod - Type of skewed-wake correction model (switch) {1=uncoupled, 2=Pitt/Peters, 3=coupled} [unused when WakeMod=0 or 3]
24
-
"default" 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]
25
-
True TipLoss - Use the Prandtl tip-loss model? (flag) [unused when WakeMod=0 or 3]
26
-
True HubLoss - Use the Prandtl hub-loss model? (flag) [unused when WakeMod=0 or 3]
27
-
True TanInd - Include tangential induction in BEMT calculations? (flag) [unused when WakeMod=0 or 3]
28
-
False AIDrag - Include the drag term in the axial-induction calculation? (flag) [unused when WakeMod=0 or 3]
29
-
False TIDrag - Include the drag term in the tangential-induction calculation? (flag) [unused when WakeMod=0,3 or TanInd=FALSE]
30
-
"Default" IndToler - Convergence tolerance for BEMT nonlinear solve residual equation {or "default"} (-) [unused when WakeMod=0 or 3]
31
-
100 MaxIter - Maximum number of iteration steps (-) [unused when WakeMod=0]
16
+
default AirDens - Air density (kg/m^3)
17
+
default KinVisc - Kinematic air viscosity (m^2/s)
18
+
default SpdSound - Speed of sound (m/s)
19
+
default Patm - Atmospheric pressure (Pa) [used only when CavitCheck=True]
20
+
default Pvap - Vapour pressure of fluid (Pa) [used only when CavitCheck=True]
21
+
====== Blade-Element/Momentum Theory Options ====================================================== [used only when WakeMod=1]
22
+
2 SkewMod - Type of skewed-wake correction model (switch) {1=uncoupled, 2=Pitt/Peters, 3=coupled} [used only when WakeMod=1]
23
+
"default" SkewModFactor - Constant used in Pitt/Peters skewed wake model {or "default" is 15/32*pi} (-) [used only when SkewMod=2; unused when WakeMod=0]
24
+
True TipLoss - Use the Prandtl tip-loss model? (flag) [used only when WakeMod=1]
25
+
False HubLoss - Use the Prandtl hub-loss model? (flag) [used only when WakeMod=1]
26
+
True TanInd - Include tangential induction in BEMT calculations? (flag) [used only when WakeMod=1]
27
+
False AIDrag - Include the drag term in the axial-induction calculation? (flag) [used only when WakeMod=1]
28
+
False TIDrag - Include the drag term in the tangential-induction calculation? (flag) [used only when WakeMod=1 and TanInd=TRUE]
29
+
"default" IndToler - Convergence tolerance for BEMT nonlinear solve residual equation {or "default"} (-) [used only when WakeMod=1]
30
+
100 MaxIter - Maximum number of iteration steps (-) [used only when WakeMod=1]
32
31
====== Dynamic Blade-Element/Momentum Theory Options ============================================== [used only when WakeMod=2]
33
32
2 DBEMT_Mod - Type of dynamic BEMT (DBEMT) model {1=constant tau1, 2=time-dependent tau1} (-) [used only when WakeMod=2]
34
33
4 tau1_const - Time constant for DBEMT (s) [used only when WakeMod=2 and DBEMT_Mod=1]
35
34
====== OLAF -- cOnvecting LAgrangian Filaments (Free Vortex Wake) Theory Options ================== [used only when WakeMod=3]
36
-
"unused" OLAFInputFileName - Input file for OLAF [used only when WakeMod=3]
35
+
"unused" OLAFInputFileName - Input file for OLAF [used only when WakeMod=3]
37
36
====== Beddoes-Leishman Unsteady Airfoil Aerodynamics Options ===================================== [used only when AFAeroMod=2]
38
-
3 UAMod - Unsteady Aero Model Switch (switch) {1=Baseline model (Original), 2=Gonzalez's variant (changes in Cn,Cc,Cm), 3=Minnema/Pierce variant (changes in Cc and Cm)} [used only when AFAeroMod=2]
37
+
3 UAMod - Unsteady Aero Model Switch (switch) {1=Baseline model (Original), 2=Gonzalez�s variant (changes in Cn,Cc,Cm), 3=Minemma/Pierce variant (changes in Cc and Cm)} [used only when AFAeroMod=2]
39
38
True FLookup - Flag to indicate whether a lookup for f' will be calculated (TRUE) or whether best-fit exponential equations will be used (FALSE); if FALSE S1-S4 must be provided in airfoil input files (flag) [used only when AFAeroMod=2]
40
39
====== Airfoil Information =========================================================================
41
40
1 AFTabMod - Interpolation method for multiple airfoil tables {1=1D interpolation on AoA (first table only); 2=2D interpolation on AoA and Re; 3=2D interpolation on AoA and UserProp} (-)
0 commit comments