24-Bld-A1 Elementary Structural Analysis · December 2017
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
National Exams December 2017 — 07-BLD-A1 Elementary Structural Analysis, 3 hours, closed book. Answer ALL of Questions 1–5; answer ONLY ONE of Questions 6, 7 or 8 (this solution set, per pipeline convention, answers all three optional questions).
Reference texts: Hibbeler, Structural Analysis, 10th ed.; Kassimali, Structural Analysis, 6th ed.
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. Bottom chord L1–L5 on a 24 m baseline (4 panels @ 6 m); pin at L2 (x=6 m), roller at L4 (x=18 m); L1 and L5 are 6 m free overhangs. Top chord U1, U2, U3 (over L2, L3, L4) at 4.5 m, with fan diagonals L1-U1, U1-L3, U2-L4, L5-U3.
Find. Influence-line ordinates for U1-U2, U2-L3, U2-L4 for a unit load at each bottom-chord joint.
Approach. A truss influence line is piecewise linear between adjacent bottom-chord joints, so it is enough to place a unit load at each joint L1–L5 and solve the (still-determinate) truss by method of sections/joints each time.
| Load at | U1-U2 | U2-L3 | U2-L4 |
|---|---|---|---|
| L1 (x=0) | +0.667 | −0.500 | +0.833 |
| L2 (x=6, support) | 0 | 0 | 0 |
| L3 (x=12) | −0.667 | +0.500 | −0.833 |
| L4 (x=18, support) | 0 | 0 | 0 |
| L5 (x=24) | +0.667 | +0.500 | −0.833 |
Connecting these five ordinates with straight lines gives each influence line. Maximum tension/compression coefficients:
| Member | Max tension | Max compression |
|---|---|---|
| U1-U2 | +2/3 = 0.667 (load at L1 or L5) | −2/3 = 0.667 (load at L3) |
| U2-L3 | +1/2 = 0.500 (load at L3 or L5) | −1/2 = 0.500 (load at L1) |
| U2-L4 | +5/6 = 0.833 (load at L1) | −5/6 = 0.833 (load at L3 or L5) |
Given. Beam: pin at x=0, roller at x=20 m, free overhang tip at x=24 m; Section 1-1 at x=6 m. Vehicle: three axles 40, 40, 20 kN, spaced 2 m then 4 m, crossing left to right.
Find. Ordinates of the IL for shear at Section 1-1, and the maximum shear there as the vehicle crosses.
Approach. For a unit load at position x on a simply-supported span of length L=20 m with a right overhang, $$V_{1\text{-}1}(x)=-x/L$$ for x left of the section and $$V_{1\text{-}1}(x)=(L-x)/L$$ for x at or right of the section (valid on the overhang too). Slide the 3-axle group across and evaluate the sum $$\Sigma P_i\,V(x_i)$$ at each position where an axle sits exactly at the section (the only candidates for an extremum, since the IL has constant slope $$-1/20$$ apart from the unit jump at x=6).
| Quantity | Value |
|---|---|
| IL ordinate just left of section | −0.30 |
| IL ordinate just right of section | +0.70 |
| Maximum shear at Section 1-1 | +60.0 kN |
| Minimum shear at Section 1-1 | −12.0 kN |