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, 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 speed CL is 1.6

* Make sure you have rules for that EXACT velocity is for minimum power and minimum thrust required.

* Use the following data.

Total engine HP @SL (180)

BSFC (lb/(HP*hr)) (0.438)

Take-off Weight (lb) (2550)

Usable Fuel (lb) (318)

Wing Area (ft^2) (174)

Swet/Serf (3.68)

Span (ft) (36.1)

CD0 (0.0331)

e (0.8252)

Propeller efficiency (0.8)

Calculate maximum range and endurance at sea level and at 8000 ft. Assume you can use all fuel and that the engine power is proportional to air 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 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