Consider the wing channel in (Figure 1) with h = 3.4 in. Neglect the effect of rounded corners. The material has a uniform thickness of 0.5 in. Figure 1 of 1 -3 in. 2 in. 2 in., 3 in. Part A Determine which locates the centroid C of the cross-sectional area of the wing chan Express your answer in inches to three significant figures. V o 41 ve ? in. Submit Request Answer Part B Determine the moment of inertia I about the centroidal z' axis. Express your answer in inches to the fourth power to three significant figures. 15| ΑΣΦ ↓↑ vec ? Ī₂ = Submit Request Answer / Daturn to Annianmant ♥ Dravide Condhank in
Consider the wing channel in (Figure 1) with h = 3.4 in. Neglect the effect of rounded corners. The material has a uniform thickness of 0.5 in. Figure 1 of 1 -3 in. 2 in. 2 in., 3 in. Part A Determine which locates the centroid C of the cross-sectional area of the wing chan Express your answer in inches to three significant figures. V o 41 ve ? in. Submit Request Answer Part B Determine the moment of inertia I about the centroidal z' axis. Express your answer in inches to the fourth power to three significant figures. 15| ΑΣΦ ↓↑ vec ? Ī₂ = Submit Request Answer / Daturn to Annianmant ♥ Dravide Condhank in
International Edition---engineering Mechanics: Statics, 4th Edition
4th Edition
ISBN:9781305501607
Author:Andrew Pytel And Jaan Kiusalaas
Publisher:Andrew Pytel And Jaan Kiusalaas
Chapter9: Moments And Products Of Inertia Of Areas
Section: Chapter Questions
Problem 9.16P: Figure (a) shows the cross-sectional dimensions for the structural steel section known as C1020...
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