The following table shows the lifting force on an aircraft wing measured in a wind tunnel at various wind velocities. Model the data with an interpolating polynomial of degree 5, and use that polynomial to estimate the lifting force at 2000 ft/s. Velocity 1 2 4 8 16 32 (100 ft/s) Lifting Force (100 lb) 0 3.12 15.86 33.7 81.5 123.0

The following table shows the lifting force on an aircraft wing measured in a wind tunnel at various wind velocities. Model the data with an interpolating polynomial of degree 5, and use that polynomial to estimate the lifting force at 2000 ft/s. Velocity 1 2 4 8 16 32 (100 ft/s) Lifting Force (100 lb) 0 3.12 15.86 33.7 81.5 123.0

Algebra & Trigonometry with Analytic Geometry

13th Edition

ISBN:9781133382119

Author:Swokowski

Publisher:Swokowski

Chapter4: Polynomial And Rational Functions

Section4.3: Zeros Of Polynomials

Problem 65E

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