Consider the wing channel in (Figure 1) with h = 4.4 in. Neglect the effect of rounded corners. The material has a unifo

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Consider the wing channel in (Figure 1) with h = 4.4 in. Neglect the effect of rounded corners. The material has a unifo

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Consider The Wing Channel In Figure 1 With H 4 4 In Neglect The Effect Of Rounded Corners The Material Has A Unifo 1
Consider The Wing Channel In Figure 1 With H 4 4 In Neglect The Effect Of Rounded Corners The Material Has A Unifo 1 (75.78 KiB) Viewed 40 times
Consider the wing channel in (Figure 1) with h = 4.4 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. -2 in. 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. y = 1.94 in. Submit Previous Answers ✓ 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. AΣo↓ vec ? Ī= 13.0 in4 Submit Previous Answers Request Answer X Incorrect; Try Again; 5 attempts remaining Provide Feedback Correct < Return to Assignment
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