ASCI 309 Exercise 3 Lift and Airfoils
Estimate the Airspeed required to support the Maximum Gross Weight of your selected airplane (from 11. above) at an Altitude of 10000 ft and flying at the given AOA of 5°. (As initially indicated, a more detailed table/Excel worksheet is beneficial to precision for this task. To support the Weight of any aircraft in level flight, an equal amount of Lift has to be generated – therefore, you can also algebraically develop the lift equation to yield a precise Airspeed result, i.e. substituting L=W and solving for V in the lift equation. Remember that conditions in this question are not at sea level.)
Max Gross weight: 6,750 lbs
Please show me the math on how you came to an answer.