Describe the solution of the given problem
Problem 1- What is the Lift on a wing that has the following conditions?
Airspeed = 180 KTAS
Altitude = 10,000 ft
Wing Area = 1000 ft2
Coefficient of Lift = 0.8
Standard Day Conditions
Problem 2- Describe the characteristics of laminar airflow in the boundary layer. Explain in brief of the above problem.