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Consider the wing channel in (Figure 1) with h = 2.8 in. Neglect the effect of rounded corners. The material has a unifo

Posted: Wed Jun 08, 2022 6:44 am
by answerhappygod
Consider The Wing Channel In Figure 1 With H 2 8 In Neglect The Effect Of Rounded Corners The Material Has A Unifo 1
Consider The Wing Channel In Figure 1 With H 2 8 In Neglect The Effect Of Rounded Corners The Material Has A Unifo 1 (5.48 KiB) Viewed 67 times
Consider the wing channel in (Figure 1) with h = 2.8 in. Neglect the effect of rounded corners. The material has a uniform thickness of 0.5 in.

Figure -2 in.. 1.5 in. 1.5 in., C 2 in.. h 1 of 1

Part A Determine y which locates the centroid C of the cross-sectional area of the wing channel. Express your answer in inches to three significant figures. IVE ΑΣΦ 41 vec ? Submit Request Answer Part B Determine the moment of inertia I about the centroidal a' axis. Express your answer in inches to the fourth power to three significant figures. VO Avec ? Ī₂¹ = ÍT in4 Submit Request Answer || in.