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1. Prepare Excel tables that show, for the Cessna Skyhawk at SL and 8,000 ft.: Velocity, CL, CD, Drag, CL/CD, CL^1.5/CD, R/C, Climb Angle, Glide
1. Prepare Excel tables that show, for the Cessna Skyhawk at SL and 8,000 ft.: Velocity, CL, CD, Drag, CL/CD, CL^1.5/CD, R/C, Climb Angle, Glide Angle at sea level and from stall speed to maximum speed. Assume that the maximum CL is 1.6. Make sure you have rows for the EXACT velocities for minimum power and minimum thrust required. o Use the following data: Total Engine HP @SL BSFC (Ib/(HP*hr)) Take-off Weight (lb) Usable Fuel (lb) Wing Area (ft^2) Swet/Sref Span (ft) CDO 180 0.438 2550 318 174 3.68 36.1 0.0331 0.8252 0.8 Propeller Efficiency 1. Prepare Excel tables that show, for the Cessna Skyhawk at SL and 8,000 ft.: Velocity, CL, CD, Drag, CL/CD, CL^1.5/CD, R/C, Climb Angle, Glide Angle at sea level and from stall speed to maximum speed. Assume that the maximum CL is 1.6. Make sure you have rows for the EXACT velocities for minimum power and minimum thrust required. o Use the following data: Total Engine HP @SL BSFC (Ib/(HP*hr)) Take-off Weight (lb) Usable Fuel (lb) Wing Area (ft^2) Swet/Sref Span (ft) CDO 180 0.438 2550 318 174 3.68 36.1 0.0331 0.8252 0.8 Propeller Efficiency
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Database And Expert Systems Applications 15th International Conference Dexa 2004 Zaragoza Spain August 30 September 3 2004 Proceedings Lncs 3180
Authors: Fernando Galindo ,Makoto Takizawa ,Roland Traunmuller
2004th Edition
3540229361, 978-3540229360
