Question: Please include all process and explanation, much appreciated! Prepare Excel tables that show, for the Cessna Skyhawks at SL and 8,000 ft: Velocity, CL, CD,
D , RUC Climbingle, Gide Angle sea level and from s peed to maximum speed 1. Prepare Excel the show, for the Cessna Skyhawks and 8000 V C L CD. Drag CUCD, C Assume that the maximum CLS 1.6 . Make sure you have rows for the EXACT velocities for minimum power and thustruired Total EngineHPOSL BSFC (HP Take-off Weight (t) Usb Full) Wing Area (2) Sweet 00331 08252 Propelerciency 2. Calculate macum Range and Endurance at selve and at 8.000 TL Assume you can use all and that engine power is proportional tow density D , RUC Climbingle, Gide Angle sea level and from s peed to maximum speed 1. Prepare Excel the show, for the Cessna Skyhawks and 8000 V C L CD. Drag CUCD, C Assume that the maximum CLS 1.6 . Make sure you have rows for the EXACT velocities for minimum power and thustruired Total EngineHPOSL BSFC (HP Take-off Weight (t) Usb Full) Wing Area (2) Sweet 00331 08252 Propelerciency 2. Calculate macum Range and Endurance at selve and at 8.000 TL Assume you can use all and that engine power is proportional tow density
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