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Problem 4.3. The drag (air resistance) experienced by airplanes can be simply modeled using a cubic equation in terms of velo

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Answer #1

Using least square method we obtain the required equation.

D (9) = + 4 9 + 0 0 + 9, 9 , (64, D. = D(95) , 1, 2, - , 6 , Using least square method, we have, 2, 4, 4 6 1 4 4 4 4 Dys, = 4A H B C D Ε F к v o v^2 v^3 v^4 V^5 V^6 Dv Dv^2 Dv^3 150 7424 22500 3375000506250000 75937500000 11390625000000 1113600 16704

Using above table we have, 247501 = 6ao + 1475a1 + 405625a2 + 123359375a3 81342500 = 1475a0 + 405625a1 + 123359375a2 + 406503

Solving this system, we get,

ao = 2038, a1 = -11.875, a2 = 0.014331, az = 0.0020021

Therefore required equation is

D(v) = 2038 - 11.875v +0.014331v2 + 0.002002103

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