CI Avery common structural component of an aircraft wing is its spar. An I shaped spar is shown in Fig. 1c. Determine the moment of inertia of this I'-shaped spar about its centroid x'- axis shown...


CI Avery common structural component of an aircraft wing is<br>its spar. An I shaped spar is shown in Fig. 1c. Determine<br>the moment of inertia of this I'-shaped spar about its<br>centroid x'- axis shown below. The spar is only symmetrical<br>about its centroid y' axis. All dimensions are in millimetres.<br>(Hint: locate the centroid first)<br>200<br>20<br>300<br>10<br>Fig, 1c<br>10<br>100<br>

Extracted text: CI Avery common structural component of an aircraft wing is its spar. An I shaped spar is shown in Fig. 1c. Determine the moment of inertia of this I'-shaped spar about its centroid x'- axis shown below. The spar is only symmetrical about its centroid y' axis. All dimensions are in millimetres. (Hint: locate the centroid first) 200 20 300 10 Fig, 1c 10 100

Jun 11, 2022
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