Calculating Q (first moment of inertia) above and below the neutral axis

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SUMMARY

The discussion focuses on calculating the first moment of inertia (Q) above and below the neutral axis for a cross-sectional area composed of two 10"x1" plates. The user initially calculated Q above as 21.31 and Q below as 30.03, leading to an inconsistency. The error was identified as using the incorrect distance from the centroid to the neutral axis for the Q above calculation, which should be 3.875" instead of 2.75". This correction aligns the values of Q above and below the neutral axis.

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  • Understanding of first moment of inertia (Q)
  • Familiarity with neutral axis concepts in structural engineering
  • Knowledge of centroid calculations for composite shapes
  • Basic principles of mechanics of materials
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tn3003
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Homework Statement



This is the cross sectional are of the shape: http://img38.imageshack.us/i/shapep.jpg/"
It's made of 2 10"x1" plates. (Picture is not to scale)

Q (first moment of inertia) above and below the neutral axis should be the same. For some reasons, my calculated Q above is not equal to Q below the NA.


The Attempt at a Solution



Taking the datum at the bottom

y bar = (10*0.5 + 10*6) / (20) = 3.25"

Q above = 7.75 * 2.75 = 21.31

Q below = 2.25 * (2.25/2) + 10 * 2.75 = 30.03

21.31 =/= 30.03

Someone please point out my mistake.
 
Last edited by a moderator:
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Your Q below is corect, but in calculating thte Q above, the distance from the centroid to the N.A. is not 2.75. I think you may have just written down the wrong number.
 
OK I see it now. The distance for Q above should be 7.75"/2 = 3.875"
I was using the centroid of the whole shape, which gave me 7.75" - 5" = 2.75" and that's wrong.

Thank you PhanthomJay for not giving out the answer and let me figure it out myself. I really appreciate it.
 
Last edited:

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