Questions
How do you find the moment of inertia of an I-section?
Split it into two flanges and a web. Each plate’s own Ī is bh³/12. The flanges are far from the neutral axis, so their A·d² terms carry most of I_x′. Add every plate’s Ī and A·d².
How do you find the centroid of a T-section?
The vertical axis of symmetry holds the centroid, so only Ȳ is needed: Ȳ = (A₁ȳ₁ + A₂ȳ₂) ÷ (A₁ + A₂) with ȳ measured from one edge, usually the bottom of the stem.
Why is I_y′ of an I-section just the sum of Ī_y?
Every plate is centred on the vertical axis of symmetry, so each d_x is zero and the parallel-axis terms vanish. The same holds for a T-section.
Which side is cubed in bh³/12?
The side across the axis. For I_x′ of a flange 120 wide and 20 thick, b = 120 and h = 20; about the y axis the 120 is cubed instead.
Are these real steel sections?
No. They are invented plates with square corners and no fillets, for exam practice. Real rolled sections have published properties. Educational practice only: not for designing or checking real structures.
How do I give my class the same problems?
Press Share with class and send the link: everyone gets the same set code and sections. Print makes up to 30 different copies, each with its own answer key.
Sources, checked 2 November 2026: Baker and Haynes, Engineering Statics: Open and Interactive, 7.5 Centroids using composite parts (holes as negative areas), Table C.1.1 Centroids of common shapes, Table C.2.1 Moments of inertia of common shapes and 10.4 Moment of inertia of composite shapes. The same formulas are on the inside covers of Hibbeler and of Beer and Johnston.