Consider the data relative to the Beech 99 aircraft in Appendixes B and C. Use the provided drawings to extract all the relevant geometric characteristics of the aircraft. This aircraft features stabilators for trimming and elevators for maneuver purposes. Assume Using the modeling outlined in this chapter, find a numerical v-alue for the following aerodynamic parameters:
Next, compare the obtained values with the true values listed in Appendix B (Aircraft 3) and evaluate the error associated with the use of the empirical modeling approach.
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