This preview shows pages 1–3. Sign up to view the full content.
This preview has intentionally blurred sections. Sign up to view the full version.View Full Document
Unformatted text preview: Pnet (lb/ft) Lift (lb) Lift Co-efficient 5.876 3.702 2.174 2.13 0.586 NACA 0015 Airfoil Pst (inches of water) Tunnel Velocity (ft/s) Fan Speed (RPM) Chordwise Distance (mm) Chordwise Distance (% of Chord) Upper Surface Pressure (Inches of Water) Upper Surface Pressure Coefficient Lower Surface Pressure (Inches of Water) Lower Surface Pressure Coefficent 0% 20% 40% 60% 80% 100% 120%-3.0-2.5-2.0-1.5-1.0-0.5 0.0 Cp Distribution on NACA 0015 Airfoil (Angle of Attack = 12 deg) Chordwise Distance from LE (% of C) Pressure Co-eff. (Cp)...
View Full Document
- Fall '10