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 lbsAOA: .6634Please show me the math on how you came to an answer.
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