Determine which locates the centroid C of the crosssectional area of the wing channel, and then

Determine ȳ which locates the centroid C of the crosssectional area of the wing channel, and then determine the moment of inertia I̅_x′ about the centroidal x′ axis. Neglect the effect of rounded corners. The material has a uniform thickness of 0.5 in.

Transcribed Image Text:

y 2 in. 1.5 in. 1.5 in. C -2 in.. 3 in.