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Unformatted text preview: Pnet (lb/ft) Lift (lb) Lift Co-efficient 5.586 2.629 2.958 2.89 0.797 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%-3.5-3.0-2.5-2.0-1.5-1.0-0.5 0.0 Cp Distribution on NACA 0015 Airfoil (Angle of Attack = 12 deg) Chordwise Distance from LE (% of C) Pressure Co-eff. (Cp)...
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This note was uploaded on 06/17/2011 for the course COMP 1103 taught by Professor Staff during the Fall '10 term at Kennesaw.
- Fall '10