The aluminum cantilevered beam is loaded as shown. - ¹/2 Given: • L = 16.8 ft F = 2000 lb • M = 1030 ft-lb • I = 125 in ¹ B₁ = B₂ = 33 = C₁ = C₂ = number (rtol=0.01, atol=1e-05) number (rtol=0.01, atol=1e-05) number (rtol=0.01, atol=1e-05) number (rtol=0.01, atol=1e-05) number (rtol=0.01, atol=1e-05) L Write an elastic curve equation valid for the entire beam in the following form: y(x) = √/7B₁x³ + 3₂x² + B₂³ + C₁z + C₂] Place the coordinate system origin (x = 0) at the left end of the beam. Give values for the m the units listed. Determine the deflection and slope at the free end. Yright-end = number (rtol=0.01, atol=1e-05) Fright-end number (rtol=0.01, atol=1e-05) F lb ft. lb lb ft².lb ft³.lb M in

The aluminum cantilevered beam is loaded as shown. - ¹/2 Given: • L = 16.8 ft F = 2000 lb • M = 1030 ft-lb • I = 125 in ¹ B₁ = B₂ = 33 = C₁ = C₂ = number (rtol=0.01, atol=1e-05) number (rtol=0.01, atol=1e-05) number (rtol=0.01, atol=1e-05) number (rtol=0.01, atol=1e-05) number (rtol=0.01, atol=1e-05) L Write an elastic curve equation valid for the entire beam in the following form: y(x) = √/7B₁x³ + 3₂x² + B₂³ + C₁z + C₂] Place the coordinate system origin (x = 0) at the left end of the beam. Give values for the m the units listed. Determine the deflection and slope at the free end. Yright-end = number (rtol=0.01, atol=1e-05) Fright-end number (rtol=0.01, atol=1e-05) F lb ft. lb lb ft².lb ft³.lb M in

Mechanics of Materials (MindTap Course List)

9th Edition

ISBN:9781337093347

Author:Barry J. Goodno, James M. Gere

Publisher:Barry J. Goodno, James M. Gere

Chapter3: Torsion

Section: Chapter Questions

Problem 3.11.5P: A square tube section has side dimension of 20 in. arid thickness of 0.5 in. If the section is used...

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