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Instructions for implementing the false position method for root finding and estimating well depth using the time of fall and sound propagation. It includes matlab exercises for finding the zero of a function and estimating the depth of a well. Additionally, it introduces the level-flight drag approximation for an aircraft.
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DOW =
2 L/Dmax
( V 2 +
)
Here DOW is the ratio of the level-flight drag force and the weight. To maintain level-flight the engine must produce this amount of thrust (thrust equals drag). Suppose we have an aircraft with L/Dmax = 12 and T /W = .4. Find the highest possible level flight speed. You should begin by drawing a graph of (normalized) drag as a function of the level flight speed V. Your answer should include the graph, a listing of your code, and the computed speed.