Airfoil analizini doğru yaptığımı sanıyorum. MH32 kullanıyorum. Kanat oluşturup analiz ettiğimde hata alıyorum. Konfigrasyonum: Kod:Panoya kopyala 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:Panoya kopyala 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 Nerede hata yapıyorum? Hatanın çözülmesi için hangi dosyaları paylaşmalıyım sizle? @SideWinder @Jira @Çağlar0707

Hocam, gördüğün reynolds numberlarında hata alıyorsun, bu sorundan kurtulmak için xfoil Direct analizden bu reynolds numaralarını tanımlayıp analiz etmen gerekiyor sonra wing üzerinde bu değerleri çalışabilirsin.