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AirfoilCambered Camber (% Ch)3 Thickness (% Ch)8 Chord (m)2 Span (m)10 Surface Area (m2) 20 Angle of attack (deg) -5 AtmosphereStd. Earth Cp Distribution Airfoil Parameters Altitude (m)0 Density (kg/m3)1.224 Pressure (Pa)101261 Temperature (C)15 Lift Coefficient-0.216 Airspeed (km/hr) 150 Dynamic Pressure (Pa) 1036.5 Mach0.12 cl vs. Pressure Distribution P > Pamb P < Pamb
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AirfoilCambered Camber (% Ch)3 Thickness (% Ch)8 Chord (m)2 Span (m)10 Surface Area (m2) 20 Angle of attack (deg) -3.75 AtmosphereStd. Earth Airfoil Parameters Altitude (m)0 Density (kg/m3)1.224 Pressure (Pa)101261 Temperature (C)15 Lift Coefficient-0.068 Airspeed (km/hr) 150 Dynamic Pressure (Pa) 1036.5 Mach0.12 cl vs. Cp Distribution Pressure Distribution P > Pamb P < Pamb
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AirfoilCambered Camber (% Ch)3 Thickness (% Ch)8 Chord (m)2 Span (m)10 Surface Area (m2) 20 Angle of attack (deg) -3.17 AtmosphereStd. Earth Airfoil Parameters Altitude (m)0 Density (kg/m3)1.224 Pressure (Pa)101261 Temperature (C)15 Lift Coefficient0.0 Airspeed (km/hr) 150 Dynamic Pressure (Pa) 1036.5 Mach0.12 cl vs. Cp Distribution Pressure Distribution P > Pamb P < Pamb
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AirfoilCambered Camber (% Ch)3 Thickness (% Ch)8 Chord (m)2 Span (m)10 Surface Area (m2) 20 Angle of attack (deg) -2.5 AtmosphereStd. Earth Airfoil Parameters Altitude (m)0 Density (kg/m3)1.224 Pressure (Pa)101261 Temperature (C)15 Lift Coefficient0.079 Airspeed (km/hr) 150 Dynamic Pressure (Pa) 1036.5 Mach0.12 cl vs. Cp Distribution Pressure Distribution P > Pamb P < Pamb
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AirfoilCambered Camber (% Ch)3 Thickness (% Ch)8 Chord (m)2 Span (m)10 Surface Area (m2) 20 Angle of attack (deg) -1.25 AtmosphereStd. Earth Airfoil Parameters Altitude (m)0 Density (kg/m3)1.224 Pressure (Pa)101261 Temperature (C)15 Lift Coefficient0.227 Airspeed (km/hr) 150 Dynamic Pressure (Pa) 1036.5 Mach0.12 cl vs. Cp Distribution Pressure Distribution P > Pamb P < Pamb
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AirfoilCambered Camber (% Ch)3 Thickness (% Ch)8 Chord (m)2 Span (m)10 Surface Area (m2) 20 Angle of attack (deg) 0 AtmosphereStd. Earth Airfoil Parameters Altitude (m)0 Density (kg/m3)1.224 Pressure (Pa)101261 Temperature (C)15 Lift Coefficient0.374 Airspeed (km/hr) 150 Dynamic Pressure (Pa) 1036.5 Mach0.12 cl vs. Cp Distribution Pressure Distribution P > Pamb P < Pamb
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AirfoilCambered Camber (% Ch)3 Thickness (% Ch)8 Chord (m)2 Span (m)10 Surface Area (m2) 20 Angle of attack (deg) 1.25 AtmosphereStd. Earth Airfoil Parameters Altitude (m)0 Density (kg/m3)1.224 Pressure (Pa)101261 Temperature (C)15 Lift Coefficient0. 552 Airspeed (km/hr) 150 Dynamic Pressure (Pa) 1036.5 Mach0.12 cl vs. Cp Distribution Pressure Distribution P > Pamb P < Pamb
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AirfoilCambered Camber (% Ch)3 Thickness (% Ch)8 Chord (m)2 Span (m)10 Surface Area (m2) 20 Angle of attack (deg) 2.5 AtmosphereStd. Earth Airfoil Parameters Altitude (m)0 Density (kg/m3)1.224 Pressure (Pa)101261 Temperature (C)15 Lift Coefficient0.669 Airspeed (km/hr) 150 Dynamic Pressure (Pa) 1036.5 Mach0.12 cl vs. Cp Distribution Pressure Distribution P > Pamb P < Pamb
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AirfoilCambered Camber (% Ch)3 Thickness (% Ch)8 Chord (m)2 Span (m)10 Surface Area (m2) 20 Angle of attack (deg) 3.75 AtmosphereStd. Earth Airfoil Parameters Altitude (m)0 Density (kg/m3)1.224 Pressure (Pa)101261 Temperature (C)15 Lift Coefficient0.816 Airspeed (km/hr) 150 Dynamic Pressure (Pa) 1036.5 Mach0.12 cl vs. Cp Distribution Pressure Distribution P > Pamb P < Pamb
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AirfoilCambered Camber (% Ch)3 Thickness (% Ch)8 Chord (m)2 Span (m)10 Surface Area (m2) 20 Angle of attack (deg) 5.0 AtmosphereStd. Earth Airfoil Parameters Altitude (m)0 Density (kg/m3)1.224 Pressure (Pa)101261 Temperature (C)15 Lift Coefficient0.963 Airspeed (km/hr) 150 Dynamic Pressure (Pa) 1036.5 Mach0.12 cl vs. Cp Distribution Pressure Distribution P > Pamb P < Pamb
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AirfoilCambered Camber (% Ch)3 Thickness (% Ch)8 Chord (m)2 Span (m)10 Surface Area (m2) 20 Angle of attack (deg) 6.25 AtmosphereStd. Earth Airfoil Parameters Altitude (m)0 Density (kg/m3)1.224 Pressure (Pa)101261 Temperature (C)15 Lift Coefficient1.109 Airspeed (km/hr) 150 Dynamic Pressure (Pa) 1036.5 Mach0.12 cl vs. Cp Distribution Pressure Distribution P > Pamb P < Pamb
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AirfoilCambered Camber (% Ch)3 Thickness (% Ch)8 Chord (m)2 Span (m)10 Surface Area (m2) 20 Angle of attack (deg) 7.5 AtmosphereStd. Earth Airfoil Parameters Altitude (m)0 Density (kg/m3)1.224 Pressure (Pa)101261 Temperature (C)15 Lift Coefficient1.254 Airspeed (km/hr) 150 Dynamic Pressure (Pa) 1036.5 Mach0.12 cl vs. Cp Distribution Pressure Distribution P > Pamb P < Pamb
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AirfoilCambered Camber (% Ch)3 Thickness (% Ch)8 Chord (m)2 Span (m)10 Surface Area (m2) 20 Angle of attack (deg) 8.75 AtmosphereStd. Earth Airfoil Parameters Altitude (m)0 Density (kg/m3)1.224 Pressure (Pa)101261 Temperature (C)15 Lift Coefficient1.399 Airspeed (km/hr) 150 Dynamic Pressure (Pa) 1036.5 Mach0.12 cl vs. Cp Distribution Pressure Distribution P > Pamb P < Pamb RESCALE
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AirfoilCambered Camber (% Ch)3 Thickness (% Ch)8 Chord (m)2 Span (m)10 Surface Area (m2) 20 Angle of attack (deg) 10 AtmosphereStd. Earth Airfoil Parameters Altitude (m)0 Density (kg/m3)1.224 Pressure (Pa)101261 Temperature (C)15 Lift Coefficient1.544 Airspeed (km/hr) 150 Dynamic Pressure (Pa) 1036.5 Mach0.12 cl vs. Cp Distribution Pressure Distribution P > Pamb P < Pamb
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AirfoilCambered Camber (% Ch)3 Thickness (% Ch)8 Chord (m)2 Span (m)10 Surface Area (m2) 20 Angle of attack (deg) 11.25 AtmosphereStd. Earth Airfoil Parameters Altitude (m)0 Density (kg/m3)1.224 Pressure (Pa)101261 Temperature (C)15 Lift Coefficient1.674 Airspeed (km/hr) 150 Dynamic Pressure (Pa) 1036.5 Mach0.12 cl vs. Cp Distribution Pressure Distribution P > Pamb P < Pamb
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