ASCI 309 Exercise 3 Lift and Airfoils

Question # 00309325 Posted By: deasym Updated on: 06/08/2016 03:23 PM Due on: 06/10/2016
Subject Physics Topic Mechanics Tutorials:
Question
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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

AOA: .6634

Please show me the math on how you came to an answer.

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