Problem 5.1. Figure 5.12 depicts an aluminum rectangular box beam of height h = 0.30 m, width b = 0.15 box beam %3D m, flange thickness ta by two layers of unidirectional composite material of thickness te = 4 mm. The section is subjected to an axial load N1 = 600 kN. The Young's moduli for the aluminum and unidirec = 12 mm, and web thickness tw = 5 mm. The beam is reinforcec %3D %3D %3D tional composite are Ea = 73 GPa and Ec of axial stress over the cross-section and sketch the distribution around the perimeter of the section. (2) Find the magnitude and location of the maximum axial stress in the aluminum and composite layers. (3) Sketch the distribution of axial strain over the section. How does vary over the full cross-section? (4) If the allowable stress for the aluminum and unidirectiona 140 GPa, respectively. (1) Find the distribution allow Do roonectively find the maximur
Problem 5.1. Figure 5.12 depicts an aluminum rectangular box beam of height h = 0.30 m, width b = 0.15 box beam %3D m, flange thickness ta by two layers of unidirectional composite material of thickness te = 4 mm. The section is subjected to an axial load N1 = 600 kN. The Young's moduli for the aluminum and unidirec = 12 mm, and web thickness tw = 5 mm. The beam is reinforcec %3D %3D %3D tional composite are Ea = 73 GPa and Ec of axial stress over the cross-section and sketch the distribution around the perimeter of the section. (2) Find the magnitude and location of the maximum axial stress in the aluminum and composite layers. (3) Sketch the distribution of axial strain over the section. How does vary over the full cross-section? (4) If the allowable stress for the aluminum and unidirectiona 140 GPa, respectively. (1) Find the distribution allow Do roonectively find the maximur
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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