1. Calculate the aircraft stall speed given the following information.

Use the diagram on page 24 to determine the CL to use in the equation.

Aircraft Angle of Attack (AOA) = 20 degrees

Aircraft's Altitude on in standard conditions = 20,000 (Use page 5 chart)

Aircraft's wing dimension = 30 ft. by 4 ft.

Aircraft's Mass = 200 slugs

Steady Deceleration Stall TAS _________ knots

2. How fast would this airplane be flying given the following conditions?

CL = 2.0, CL Max = 2.7, Stall Speed = 120

EAS = _______ knots