Airfoil analizini doğru yaptığımı sanıyorum. MH32 kullanıyorum. Kanat oluşturup analiz ettiğimde hata alıyorum.
Konfigrasyonum:
Nerede hata yapıyorum? Hatanın çözülmesi için hangi dosyaları paylaşmalıyım sizle?
@SideWinder @Jira @Çağlar0707
Konfigrasyonum:
Kod:
Type 1: Fixed speed
VInf = 15 m/s
3D-Panels/VLM2
Using plane inertia
Mass = 0.000 kg
CoG.x = 0 m
CoG.z = 0 m
B.C. = Dirichlet
Analysis type = Viscous
Ref. dimensions = Planform
Ref. area = 0.384m²
Ref. span = 1.600m
Ref. chord = 0.240m
Density =1.225 kg/m3
Viscosity =1.5e-05m²/s
Data points = 0
Kod:
xflr5 v6.54
05.02.2022 23:07:51
Launching Analysis
Launching the 3D Panel Analysis....
plane
Type 1 - Fixed speed polar
Wings as thin surfaces
Using ring vortices - VLM2
Using Neumann boundary conditions for wings
Density = 1.225kg/m3
Viscosity = 1.5e-05m²/s
Reference Area = 0.384m²
Reference length = 1.6m
Counted 494 panel elements
Mass= 0.000 kg
___Center of Gravity Position - Body axis____
CoG_x= 0.0000 m
CoG_y= 0.0000 m
CoG_z= 0.0000 m
___Inertia - Body Axis - CoG Origin____
Ibxx= 0 kg.m²
Ibyy= 0 kg.m²
Ibzz= 0 kg.m²
Ibxz= 0 kg.m²
Solving the problem...
Creating the influence matrix...
Creating the unit RHS vectors...
Performing LU Matrix decomposition...
Solving the LU system...
Time for linear system solve: 0.069 s
Creating source strengths...
Calculating doublet strength...
Calculating aerodynamic coefficients in the far field plane
Calculating point 0.00°....
Calculating point -0.50°....
Calculating point -1.00°....
Calculating point -1.50°....
Calculating point -2.00°....
Calculating point -2.50°....
Calculating point -3.00°....
Computing On-Body Speeds...
Computing Plane for alpha= 0.00°
Calculating aerodynamic coefficients...
Calculating wing...Main Wing
Span pos = -0.80 m, Re = 230034, Cl = 0.03 is outside the flight envelope
Span pos = -0.79 m, Re = 230171, Cl = 0.06 is outside the flight envelope
Span pos = -0.78 m, Re = 230442, Cl = 0.08 is outside the flight envelope
Span pos = -0.77 m, Re = 230848, Cl = 0.10 is outside the flight envelope
Span pos = -0.74 m, Re = 231384, Cl = 0.12 is outside the flight envelope
Span pos = -0.72 m, Re = 232048, Cl = 0.14 is outside the flight envelope
Span pos = -0.69 m, Re = 232834, Cl = 0.15 is outside the flight envelope
Span pos = -0.65 m, Re = 233737, Cl = 0.16 is outside the flight envelope
Span pos = -0.61 m, Re = 234751, Cl = 0.17 is outside the flight envelope
Span pos = -0.57 m, Re = 235870, Cl = 0.18 is outside the flight envelope
Span pos = -0.52 m, Re = 237085, Cl = 0.19 is outside the flight envelope
Span pos = -0.46 m, Re = 238388, Cl = 0.19 is outside the flight envelope
Span pos = -0.41 m, Re = 239771, Cl = 0.20 is outside the flight envelope
Span pos = -0.35 m, Re = 241224, Cl = 0.20 is outside the flight envelope
Span pos = -0.29 m, Re = 242736, Cl = 0.20 is outside the flight envelope
Span pos = -0.23 m, Re = 244298, Cl = 0.20 is outside the flight envelope
Span pos = -0.16 m, Re = 245899, Cl = 0.20 is outside the flight envelope
Span pos = -0.10 m, Re = 247528, Cl = 0.20 is outside the flight envelope
Span pos = -0.03 m, Re = 249174, Cl = 0.20 is outside the flight envelope
Span pos = 0.03 m, Re = 249174, Cl = 0.20 is outside the flight envelope
Span pos = 0.10 m, Re = 247528, Cl = 0.20 is outside the flight envelope
Span pos = 0.16 m, Re = 245899, Cl = 0.20 is outside the flight envelope
Span pos = 0.23 m, Re = 244298, Cl = 0.20 is outside the flight envelope
Span pos = 0.29 m, Re = 242736, Cl = 0.20 is outside the flight envelope
Span pos = 0.35 m, Re = 241224, Cl = 0.20 is outside the flight envelope
Span pos = 0.41 m, Re = 239771, Cl = 0.20 is outside the flight envelope
Span pos = 0.46 m, Re = 238388, Cl = 0.19 is outside the flight envelope
Span pos = 0.52 m, Re = 237085, Cl = 0.19 is outside the flight envelope
Span pos = 0.57 m, Re = 235870, Cl = 0.18 is outside the flight envelope
Span pos = 0.61 m, Re = 234751, Cl = 0.17 is outside the flight envelope
Span pos = 0.65 m, Re = 233737, Cl = 0.16 is outside the flight envelope
Span pos = 0.69 m, Re = 232834, Cl = 0.15 is outside the flight envelope
Span pos = 0.72 m, Re = 232048, Cl = 0.14 is outside the flight envelope
Span pos = 0.74 m, Re = 231384, Cl = 0.12 is outside the flight envelope
Span pos = 0.77 m, Re = 230848, Cl = 0.10 is outside the flight envelope
Span pos = 0.78 m, Re = 230442, Cl = 0.08 is outside the flight envelope
Span pos = 0.79 m, Re = 230171, Cl = 0.06 is outside the flight envelope
Span pos = 0.80 m, Re = 230034, Cl = 0.03 is outside the flight envelope
Computing Plane for alpha= -0.50°
Calculating aerodynamic coefficients...
Calculating wing...Main Wing
Span pos = -0.80 m, Re = 230034, Cl = 0.03 is outside the flight envelope
Span pos = -0.79 m, Re = 230171, Cl = 0.05 is outside the flight envelope
Span pos = -0.78 m, Re = 230442, Cl = 0.07 is outside the flight envelope
Span pos = -0.77 m, Re = 230848, Cl = 0.08 is outside the flight envelope
Span pos = -0.74 m, Re = 231384, Cl = 0.10 is outside the flight envelope
Span pos = -0.72 m, Re = 232048, Cl = 0.11 is outside the flight envelope
Span pos = -0.69 m, Re = 232834, Cl = 0.12 is outside the flight envelope
Span pos = -0.65 m, Re = 233737, Cl = 0.13 is outside the flight envelope
Span pos = -0.61 m, Re = 234751, Cl = 0.14 is outside the flight envelope
Span pos = -0.57 m, Re = 235870, Cl = 0.14 is outside the flight envelope
Span pos = -0.52 m, Re = 237085, Cl = 0.15 is outside the flight envelope
Span pos = -0.46 m, Re = 238388, Cl = 0.15 is outside the flight envelope
Span pos = -0.41 m, Re = 239771, Cl = 0.15 is outside the flight envelope
Span pos = -0.35 m, Re = 241224, Cl = 0.16 is outside the flight envelope
Span pos = -0.29 m, Re = 242736, Cl = 0.16 is outside the flight envelope
Span pos = -0.23 m, Re = 244298, Cl = 0.16 is outside the flight envelope
Span pos = -0.16 m, Re = 245899, Cl = 0.16 is outside the flight envelope
Span pos = -0.10 m, Re = 247528, Cl = 0.16 is outside the flight envelope
Span pos = -0.03 m, Re = 249174, Cl = 0.16 is outside the flight envelope
Span pos = 0.03 m, Re = 249174, Cl = 0.16 is outside the flight envelope
Span pos = 0.10 m, Re = 247528, Cl = 0.16 is outside the flight envelope
Span pos = 0.16 m, Re = 245899, Cl = 0.16 is outside the flight envelope
Span pos = 0.23 m, Re = 244298, Cl = 0.16 is outside the flight envelope
Span pos = 0.29 m, Re = 242736, Cl = 0.16 is outside the flight envelope
Span pos = 0.35 m, Re = 241224, Cl = 0.16 is outside the flight envelope
Span pos = 0.41 m, Re = 239771, Cl = 0.15 is outside the flight envelope
Span pos = 0.46 m, Re = 238388, Cl = 0.15 is outside the flight envelope
Span pos = 0.52 m, Re = 237085, Cl = 0.15 is outside the flight envelope
Span pos = 0.57 m, Re = 235870, Cl = 0.14 is outside the flight envelope
Span pos = 0.61 m, Re = 234751, Cl = 0.14 is outside the flight envelope
Span pos = 0.65 m, Re = 233737, Cl = 0.13 is outside the flight envelope
Span pos = 0.69 m, Re = 232834, Cl = 0.12 is outside the flight envelope
Span pos = 0.72 m, Re = 232048, Cl = 0.11 is outside the flight envelope
Span pos = 0.74 m, Re = 231384, Cl = 0.10 is outside the flight envelope
Span pos = 0.77 m, Re = 230848, Cl = 0.08 is outside the flight envelope
Span pos = 0.78 m, Re = 230442, Cl = 0.07 is outside the flight envelope
Span pos = 0.79 m, Re = 230171, Cl = 0.05 is outside the flight envelope
Span pos = 0.80 m, Re = 230034, Cl = 0.03 is outside the flight envelope
Computing Plane for alpha= -1.00°
Calculating aerodynamic coefficients...
Calculating wing...Main Wing
Span pos = -0.80 m, Re = 230034, Cl = 0.02 is outside the flight envelope
Span pos = -0.79 m, Re = 230171, Cl = 0.04 is outside the flight envelope
Span pos = -0.78 m, Re = 230442, Cl = 0.05 is outside the flight envelope
Span pos = -0.77 m, Re = 230848, Cl = 0.06 is outside the flight envelope
Span pos = -0.74 m, Re = 231384, Cl = 0.08 is outside the flight envelope
Span pos = -0.72 m, Re = 232048, Cl = 0.08 is outside the flight envelope
Span pos = -0.69 m, Re = 232834, Cl = 0.09 is outside the flight envelope
Span pos = -0.65 m, Re = 233737, Cl = 0.10 is outside the flight envelope
Span pos = -0.61 m, Re = 234751, Cl = 0.10 is outside the flight envelope
Span pos = -0.57 m, Re = 235870, Cl = 0.10 is outside the flight envelope
Span pos = -0.52 m, Re = 237085, Cl = 0.11 is outside the flight envelope
Span pos = -0.46 m, Re = 238388, Cl = 0.11 is outside the flight envelope
Span pos = -0.41 m, Re = 239771, Cl = 0.11 is outside the flight envelope
Span pos = -0.35 m, Re = 241224, Cl = 0.11 is outside the flight envelope
Span pos = -0.29 m, Re = 242736, Cl = 0.11 is outside the flight envelope
Span pos = -0.23 m, Re = 244298, Cl = 0.11 is outside the flight envelope
Span pos = -0.16 m, Re = 245899, Cl = 0.12 is outside the flight envelope
Span pos = -0.10 m, Re = 247528, Cl = 0.11 is outside the flight envelope
Span pos = -0.03 m, Re = 249174, Cl = 0.11 is outside the flight envelope
Span pos = 0.03 m, Re = 249174, Cl = 0.11 is outside the flight envelope
Span pos = 0.10 m, Re = 247528, Cl = 0.11 is outside the flight envelope
Span pos = 0.16 m, Re = 245899, Cl = 0.12 is outside the flight envelope
Span pos = 0.23 m, Re = 244298, Cl = 0.11 is outside the flight envelope
Span pos = 0.29 m, Re = 242736, Cl = 0.11 is outside the flight envelope
Span pos = 0.35 m, Re = 241224, Cl = 0.11 is outside the flight envelope
Span pos = 0.41 m, Re = 239771, Cl = 0.11 is outside the flight envelope
Span pos = 0.46 m, Re = 238388, Cl = 0.11 is outside the flight envelope
Span pos = 0.52 m, Re = 237085, Cl = 0.11 is outside the flight envelope
Span pos = 0.57 m, Re = 235870, Cl = 0.10 is outside the flight envelope
Span pos = 0.61 m, Re = 234751, Cl = 0.10 is outside the flight envelope
Span pos = 0.65 m, Re = 233737, Cl = 0.10 is outside the flight envelope
Span pos = 0.69 m, Re = 232834, Cl = 0.09 is outside the flight envelope
Span pos = 0.72 m, Re = 232048, Cl = 0.08 is outside the flight envelope
Span pos = 0.74 m, Re = 231384, Cl = 0.08 is outside the flight envelope
Span pos = 0.77 m, Re = 230848, Cl = 0.06 is outside the flight envelope
Span pos = 0.78 m, Re = 230442, Cl = 0.05 is outside the flight envelope
Span pos = 0.79 m, Re = 230171, Cl = 0.04 is outside the flight envelope
Span pos = 0.80 m, Re = 230034, Cl = 0.02 is outside the flight envelope
Computing Plane for alpha= -1.50°
Calculating aerodynamic coefficients...
Calculating wing...Main Wing
Span pos = -0.80 m, Re = 230034, Cl = 0.02 is outside the flight envelope
Span pos = -0.79 m, Re = 230171, Cl = 0.03 is outside the flight envelope
Span pos = -0.78 m, Re = 230442, Cl = 0.04 is outside the flight envelope
Span pos = -0.77 m, Re = 230848, Cl = 0.04 is outside the flight envelope
Span pos = -0.74 m, Re = 231384, Cl = 0.05 is outside the flight envelope
Span pos = -0.72 m, Re = 232048, Cl = 0.06 is outside the flight envelope
Span pos = -0.69 m, Re = 232834, Cl = 0.06 is outside the flight envelope
Span pos = -0.65 m, Re = 233737, Cl = 0.06 is outside the flight envelope
Span pos = -0.61 m, Re = 234751, Cl = 0.06 is outside the flight envelope
Span pos = -0.57 m, Re = 235870, Cl = 0.07 is outside the flight envelope
Span pos = -0.52 m, Re = 237085, Cl = 0.07 is outside the flight envelope
Span pos = -0.46 m, Re = 238388, Cl = 0.07 is outside the flight envelope
Span pos = -0.41 m, Re = 239771, Cl = 0.07 is outside the flight envelope
Span pos = -0.35 m, Re = 241224, Cl = 0.07 is outside the flight envelope
Span pos = -0.29 m, Re = 242736, Cl = 0.07 is outside the flight envelope
Span pos = -0.23 m, Re = 244298, Cl = 0.07 is outside the flight envelope
Span pos = -0.16 m, Re = 245899, Cl = 0.07 is outside the flight envelope
Span pos = -0.10 m, Re = 247528, Cl = 0.07 is outside the flight envelope
Span pos = -0.03 m, Re = 249174, Cl = 0.07 is outside the flight envelope
Span pos = 0.03 m, Re = 249174, Cl = 0.07 is outside the flight envelope
Span pos = 0.10 m, Re = 247528, Cl = 0.07 is outside the flight envelope
Span pos = 0.16 m, Re = 245899, Cl = 0.07 is outside the flight envelope
Span pos = 0.23 m, Re = 244298, Cl = 0.07 is outside the flight envelope
Span pos = 0.29 m, Re = 242736, Cl = 0.07 is outside the flight envelope
Span pos = 0.35 m, Re = 241224, Cl = 0.07 is outside the flight envelope
Span pos = 0.41 m, Re = 239771, Cl = 0.07 is outside the flight envelope
Span pos = 0.46 m, Re = 238388, Cl = 0.07 is outside the flight envelope
Span pos = 0.52 m, Re = 237085, Cl = 0.07 is outside the flight envelope
Span pos = 0.57 m, Re = 235870, Cl = 0.07 is outside the flight envelope
Span pos = 0.61 m, Re = 234751, Cl = 0.06 is outside the flight envelope
Span pos = 0.65 m, Re = 233737, Cl = 0.06 is outside the flight envelope
Span pos = 0.69 m, Re = 232834, Cl = 0.06 is outside the flight envelope
Span pos = 0.72 m, Re = 232048, Cl = 0.06 is outside the flight envelope
Span pos = 0.74 m, Re = 231384, Cl = 0.05 is outside the flight envelope
Span pos = 0.77 m, Re = 230848, Cl = 0.04 is outside the flight envelope
Span pos = 0.78 m, Re = 230442, Cl = 0.04 is outside the flight envelope
Span pos = 0.79 m, Re = 230171, Cl = 0.03 is outside the flight envelope
Span pos = 0.80 m, Re = 230034, Cl = 0.02 is outside the flight envelope
Computing Plane for alpha= -2.00°
Calculating aerodynamic coefficients...
Calculating wing...Main Wing
Span pos = -0.80 m, Re = 230034, Cl = 0.01 is outside the flight envelope
Span pos = -0.79 m, Re = 230171, Cl = 0.01 is outside the flight envelope
Span pos = -0.78 m, Re = 230442, Cl = 0.02 is outside the flight envelope
Span pos = -0.77 m, Re = 230848, Cl = 0.02 is outside the flight envelope
Span pos = -0.74 m, Re = 231384, Cl = 0.03 is outside the flight envelope
Span pos = -0.72 m, Re = 232048, Cl = 0.03 is outside the flight envelope
Span pos = -0.69 m, Re = 232834, Cl = 0.03 is outside the flight envelope
Span pos = -0.65 m, Re = 233737, Cl = 0.03 is outside the flight envelope
Span pos = -0.61 m, Re = 234751, Cl = 0.03 is outside the flight envelope
Span pos = -0.57 m, Re = 235870, Cl = 0.03 is outside the flight envelope
Span pos = -0.52 m, Re = 237085, Cl = 0.03 is outside the flight envelope
Span pos = -0.46 m, Re = 238388, Cl = 0.03 is outside the flight envelope
Span pos = -0.41 m, Re = 239771, Cl = 0.03 is outside the flight envelope
Span pos = -0.35 m, Re = 241224, Cl = 0.03 is outside the flight envelope
Span pos = -0.29 m, Re = 242736, Cl = 0.03 is outside the flight envelope
Span pos = -0.23 m, Re = 244298, Cl = 0.03 is outside the flight envelope
Span pos = -0.16 m, Re = 245899, Cl = 0.03 is outside the flight envelope
Span pos = -0.10 m, Re = 247528, Cl = 0.03 is outside the flight envelope
Span pos = -0.03 m, Re = 249174, Cl = 0.03 is outside the flight envelope
Span pos = 0.03 m, Re = 249174, Cl = 0.03 is outside the flight envelope
Span pos = 0.10 m, Re = 247528, Cl = 0.03 is outside the flight envelope
Span pos = 0.16 m, Re = 245899, Cl = 0.03 is outside the flight envelope
Span pos = 0.23 m, Re = 244298, Cl = 0.03 is outside the flight envelope
Span pos = 0.29 m, Re = 242736, Cl = 0.03 is outside the flight envelope
Span pos = 0.35 m, Re = 241224, Cl = 0.03 is outside the flight envelope
Span pos = 0.41 m, Re = 239771, Cl = 0.03 is outside the flight envelope
Span pos = 0.46 m, Re = 238388, Cl = 0.03 is outside the flight envelope
Span pos = 0.52 m, Re = 237085, Cl = 0.03 is outside the flight envelope
Span pos = 0.57 m, Re = 235870, Cl = 0.03 is outside the flight envelope
Span pos = 0.61 m, Re = 234751, Cl = 0.03 is outside the flight envelope
Span pos = 0.65 m, Re = 233737, Cl = 0.03 is outside the flight envelope
Span pos = 0.69 m, Re = 232834, Cl = 0.03 is outside the flight envelope
Span pos = 0.72 m, Re = 232048, Cl = 0.03 is outside the flight envelope
Span pos = 0.74 m, Re = 231384, Cl = 0.03 is outside the flight envelope
Span pos = 0.77 m, Re = 230848, Cl = 0.02 is outside the flight envelope
Span pos = 0.78 m, Re = 230442, Cl = 0.02 is outside the flight envelope
Span pos = 0.79 m, Re = 230171, Cl = 0.01 is outside the flight envelope
Span pos = 0.80 m, Re = 230034, Cl = 0.01 is outside the flight envelope
Computing Plane for alpha= -2.50°
Calculating aerodynamic coefficients...
Calculating wing...Main Wing
Span pos = -0.80 m, Re = 230034, Cl = 0.00 is outside the flight envelope
Span pos = -0.79 m, Re = 230171, Cl = 0.00 is outside the flight envelope
Span pos = -0.78 m, Re = 230442, Cl = 0.01 is outside the flight envelope
Span pos = -0.77 m, Re = 230848, Cl = 0.00 is outside the flight envelope
Span pos = -0.74 m, Re = 231384, Cl = 0.00 is outside the flight envelope
Span pos = -0.72 m, Re = 232048, Cl = 0.00 is outside the flight envelope
Span pos = -0.69 m, Re = 232834, Cl = -0.00 is outside the flight envelope
Span pos = -0.65 m, Re = 233737, Cl = -0.00 is outside the flight envelope
Span pos = -0.61 m, Re = 234751, Cl = -0.01 is outside the flight envelope
Span pos = -0.57 m, Re = 235870, Cl = -0.01 is outside the flight envelope
Span pos = -0.52 m, Re = 237085, Cl = -0.01 is outside the flight envelope
Span pos = -0.46 m, Re = 238388, Cl = -0.01 is outside the flight envelope
Span pos = -0.41 m, Re = 239771, Cl = -0.01 is outside the flight envelope
Span pos = -0.35 m, Re = 241224, Cl = -0.02 is outside the flight envelope
Span pos = -0.29 m, Re = 242736, Cl = -0.02 is outside the flight envelope
Span pos = -0.23 m, Re = 244298, Cl = -0.02 is outside the flight envelope
Span pos = -0.16 m, Re = 245899, Cl = -0.02 is outside the flight envelope
Span pos = -0.10 m, Re = 247528, Cl = -0.02 is outside the flight envelope
Span pos = -0.03 m, Re = 249174, Cl = -0.02 is outside the flight envelope
Span pos = 0.03 m, Re = 249174, Cl = -0.02 is outside the flight envelope
Span pos = 0.10 m, Re = 247528, Cl = -0.02 is outside the flight envelope
Span pos = 0.16 m, Re = 245899, Cl = -0.02 is outside the flight envelope
Span pos = 0.23 m, Re = 244298, Cl = -0.02 is outside the flight envelope
Span pos = 0.29 m, Re = 242736, Cl = -0.02 is outside the flight envelope
Span pos = 0.35 m, Re = 241224, Cl = -0.02 is outside the flight envelope
Span pos = 0.41 m, Re = 239771, Cl = -0.01 is outside the flight envelope
Span pos = 0.46 m, Re = 238388, Cl = -0.01 is outside the flight envelope
Span pos = 0.52 m, Re = 237085, Cl = -0.01 is outside the flight envelope
Span pos = 0.57 m, Re = 235870, Cl = -0.01 is outside the flight envelope
Span pos = 0.61 m, Re = 234751, Cl = -0.01 is outside the flight envelope
Span pos = 0.65 m, Re = 233737, Cl = -0.00 is outside the flight envelope
Span pos = 0.69 m, Re = 232834, Cl = -0.00 is outside the flight envelope
Span pos = 0.72 m, Re = 232048, Cl = 0.00 is outside the flight envelope
Span pos = 0.74 m, Re = 231384, Cl = 0.00 is outside the flight envelope
Span pos = 0.77 m, Re = 230848, Cl = 0.00 is outside the flight envelope
Span pos = 0.78 m, Re = 230442, Cl = 0.01 is outside the flight envelope
Span pos = 0.79 m, Re = 230171, Cl = 0.00 is outside the flight envelope
Span pos = 0.80 m, Re = 230034, Cl = 0.00 is outside the flight envelope
Computing Plane for alpha= -3.00°
Calculating aerodynamic coefficients...
Calculating wing...Main Wing
Span pos = -0.80 m, Re = 230034, Cl = -0.00 is outside the flight envelope
Span pos = -0.79 m, Re = 230171, Cl = -0.01 is outside the flight envelope
Span pos = -0.78 m, Re = 230442, Cl = -0.01 is outside the flight envelope
Span pos = -0.77 m, Re = 230848, Cl = -0.02 is outside the flight envelope
Span pos = -0.74 m, Re = 231384, Cl = -0.02 is outside the flight envelope
Span pos = -0.72 m, Re = 232048, Cl = -0.03 is outside the flight envelope
Span pos = -0.69 m, Re = 232834, Cl = -0.03 is outside the flight envelope
Span pos = -0.65 m, Re = 233737, Cl = -0.04 is outside the flight envelope
Span pos = -0.61 m, Re = 234751, Cl = -0.04 is outside the flight envelope
Span pos = -0.57 m, Re = 235870, Cl = -0.05 is outside the flight envelope
Span pos = -0.52 m, Re = 237085, Cl = -0.05 is outside the flight envelope
Span pos = -0.46 m, Re = 238388, Cl = -0.05 is outside the flight envelope
Span pos = -0.41 m, Re = 239771, Cl = -0.06 is outside the flight envelope
Span pos = -0.35 m, Re = 241224, Cl = -0.06 is outside the flight envelope
Span pos = -0.29 m, Re = 242736, Cl = -0.06 is outside the flight envelope
Span pos = -0.23 m, Re = 244298, Cl = -0.06 is outside the flight envelope
Span pos = -0.16 m, Re = 245899, Cl = -0.06 is outside the flight envelope
Span pos = -0.10 m, Re = 247528, Cl = -0.06 is outside the flight envelope
Span pos = -0.03 m, Re = 249174, Cl = -0.06 is outside the flight envelope
Span pos = 0.03 m, Re = 249174, Cl = -0.06 is outside the flight envelope
Span pos = 0.10 m, Re = 247528, Cl = -0.06 is outside the flight envelope
Span pos = 0.16 m, Re = 245899, Cl = -0.06 is outside the flight envelope
Span pos = 0.23 m, Re = 244298, Cl = -0.06 is outside the flight envelope
Span pos = 0.29 m, Re = 242736, Cl = -0.06 is outside the flight envelope
Span pos = 0.35 m, Re = 241224, Cl = -0.06 is outside the flight envelope
Span pos = 0.41 m, Re = 239771, Cl = -0.06 is outside the flight envelope
Span pos = 0.46 m, Re = 238388, Cl = -0.05 is outside the flight envelope
Span pos = 0.52 m, Re = 237085, Cl = -0.05 is outside the flight envelope
Span pos = 0.57 m, Re = 235870, Cl = -0.05 is outside the flight envelope
Span pos = 0.61 m, Re = 234751, Cl = -0.04 is outside the flight envelope
Span pos = 0.65 m, Re = 233737, Cl = -0.04 is outside the flight envelope
Span pos = 0.69 m, Re = 232834, Cl = -0.03 is outside the flight envelope
Span pos = 0.72 m, Re = 232048, Cl = -0.03 is outside the flight envelope
Span pos = 0.74 m, Re = 231384, Cl = -0.02 is outside the flight envelope
Span pos = 0.77 m, Re = 230848, Cl = -0.02 is outside the flight envelope
Span pos = 0.78 m, Re = 230442, Cl = -0.01 is outside the flight envelope
Span pos = 0.79 m, Re = 230171, Cl = -0.01 is outside the flight envelope
Span pos = 0.80 m, Re = 230034, Cl = -0.00 is outside the flight envelope
Panel Analysis completed ... Errors encountered
@SideWinder @Jira @Çağlar0707