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04-BS-6 · December 2014

Question 6 of 8: Eccentric & Inclined Load on a Column

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

04-BS-6: Mechanics of Materials — National Exams, December 2014

3 hours duration. Closed book (one hand-written aid sheet permitted). Any FIVE of the eight questions constitute a complete paper; all eight are solved below as a complete study resource.

Reference texts: Hibbeler, Mechanics of Materials, 10th ed.; Beer, Johnston, DeWolf & Mazurek, Mechanics of Materials, 7th ed.; Gere & Goodno, Mechanics of Materials, 8th ed.

Question 6: Eccentric & Inclined Load on a Column (20 marks)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

Given.

Eccentric axial load600 kN, vertical, e=250 mm from the column centreline
Inclined load80 kN on a collar, 3-4-5 slope (down and to the left), applied at the column’s left face, 300 mm above section a-a
Section a-a200 mm (in-plane) × 50 mm rectangle
Materialσyield=400 MPa, E=200 GPa

Find. (a) the normal stress distribution at section a-a (max/min); (b) the shear stress distribution at section a-a (max/min). Ignore column buckling.

600 kN250 mm80 kNa-a300 mm200 mm50 mmSection a-a
Column with the 600 kN eccentric load, the 80 kN inclined (3-4-5) collar load, and section a-a 300 mm below the collar.

Approach. Reduce every force above section a-a to an equivalent axial force, bending moment, and shear force AT the section, then superpose σ=P/A±My/I and τ=1.5V/A (rectangular section).

  1. Resolve the 80 kN load (3-4-5 slope): $$F_x=-80\left(\tfrac{4}{5}\right)=-64\text{ kN (left)},\qquad F_z=-80\left(\tfrac{3}{5}\right)=-48\text{ kN (down)}.$$
  2. Total axial (compressive) force at a-a: $$P_{total}=600+48=648\text{ kN}.$$
  3. Total bending moment about the section centroid (moment increases compression on the +x/eccentricity side): from the 600 kN load, $M_1=600(250)=150{,}000$ kN·mm; from the 80 kN load's vertical component at x=−100 mm, $M_2=48(-100)/1000\cdot1000=-4800$ kN·mm... combining with the horizontal component acting at 300 mm above the section, $$M=e P_{600} + \left(z_{80}F_{x,80}-x_{80}F_{z,80}\right)=1.260e+08\text{ N}\cdot\text{mm} = 126.0\text{ kN}\cdot\text{m}.$$
  4. Section properties (bending about the axis perpendicular to the 250 mm eccentricity, i.e. about the 50 mm-thick axis): $$A=10000\text{ mm}^2,\qquad I=\dfrac{(50)(200)^3}{12}=3.333e+07\text{ mm}^4,\qquad c=100\text{ mm}.$$
  5. Normal stress distribution $\sigma=P/A+Mx/I$ (compression positive): $$\boxed{\sigma_{max}=442.8\text{ MPa (compression, at the eccentric-load side)}}$$ $$\boxed{\sigma_{min}=-313.2\text{ MPa}}$$ (i.e. 313.2 MPa tension at the opposite edge — the 250 mm eccentricity lies far outside the section’s kern, so the far edge goes into net tension; the compressive peak exceeds the 400 MPa yield, worth flagging as a design concern even though the question only asks for the linear-elastic distribution).
  6. Shear stress distribution. Only the 80 kN load’s horizontal component is a transverse (shear) force on this horizontal cut: $$V=64\text{ kN}.$$ For a rectangle, shear is parabolic, zero at the edges and maximum at the centroid: $$\boxed{\tau_{max}=\dfrac{1.5V}{A}=9.60\text{ MPa (at the centroidal axis)}},\qquad \tau=0\text{ at }x=\pm100\text{ mm.}$$
QuantityValue
Total axial force at a-a648 kN (compression)
Bending moment at a-a126.0 kN·m
σmax (eccentric side)442.8 MPa (compression)
σmin (far side)313.2 MPa (tension)
τmax (centroid)9.60 MPa