---
title: "Truss ILDs for AB, BC, BG, lower chord"
subject: "Theory of Structures I"
chapter: 5
key: "semester_4/theory_of_structures_i:truss-ild-ab-bc-bg-lower-chord"
source: https://www.bctengineer.com/q/semester_4/theory_of_structures_i/truss-ild-ab-bc-bg-lower-chord
site: BCT Engineering
---

# Truss ILDs for AB, BC, BG, lower chord

Theory of Structures I · Chapter 5: Influence Lines for Simple Structures

- Asked in: 2068 Bhadra, 8 marks
- Answer checked by Claude Opus 5.5 (high effort) on 2026-10-14
- Page: https://www.bctengineer.com/q/semester_4/theory_of_structures_i/truss-ild-ab-bc-bg-lower-chord
- Whole chapter: https://www.bctengineer.com/md/semester_4/theory_of_structures_i/chapter-5

## Question

Draw influence line diagrams for the forces in members AB, BC and BG of the truss. The load moves in the lower chord of the truss. [Figure: truss with A (hinge) and E (roller); bottom joints A, F, G, H, E, 4 panels of 15 m = 60 m; B and D 5 m above the bottom chord, apex C 10 m above; verticals BF, CG, DH and diagonals BG, GD.]

## Short answer

ILD ordinates: AB compression, 0 at A, peak −2.372 at F, then to 0 at E; BC compression, peak −1.581 at G; BG compression in panel AF, peak −1.581 at F, zero for loads beyond G. All shapes are piecewise linear.

## Answer

**Data:** bottom chord $A$–$F$–$G$–$H$–$E$, 4 panels of 15 m (span 60 m); $B$, $D$ are 5 m and $C$ is 10 m above the bottom chord; verticals $BF$, $CG$, $DH$; diagonals $BG$, $GD$. $A$ hinge, $E$ roller. The load moves on the lower chord. Reactions: $R_A = \dfrac{60-x}{60}$, $R_E = \dfrac{x}{60}$. $AB$ and $BC$ both have slope $\tfrac13$ (so $A$, $B$, $C$ are collinear).

#### Member AB
Joint $A$: vertical equilibrium, $F_{AB}\sin\alpha = -R_A$ with $\sin\alpha = \dfrac{5}{15.81} = 0.316$. So $F_{AB} = -3.162\,R_A$ (compression); the load at $A$ goes straight to the support, so the ordinate at $A$ is 0.

#### Member BC
Section through $BC$, $BG$, $FG$; moments about $G$ (lever arm of $BC$: $\dfrac{30}{\sqrt{10}} = 9.487$ m).

- Load right of $G$: $F_{BC} = -\dfrac{30R_A}{9.487} = -3.162R_A$.
- Load left of $F$: $F_{BC} = -3.162R_E$.

#### Member BG
Moments about $A$ (where $BC$ and $FG$ meet; lever arm of $BG$ = 9.49 m).

- Load right of $G$: $F_{BG} = 0$ (the left part has only $R_A$, which passes through $A$).
- Load left of $F$: $F_{BG} = -\dfrac{60R_E}{9.49} = -6.325R_E$.

#### Ordinates (per unit load; + tension, − compression)
| Member | A | F | G | H | E |
|---|---|---|---|---|---|
| AB | 0.000 | -2.372 | -1.581 | -0.791 | 0.000 |
| BC | 0.000 | -0.791 | -1.581 | -0.791 | 0.000 |
| BG | 0.000 | -1.581 | 0.000 | 0.000 | 0.000 |

#### Shapes
- **AB:** compression, 0 at $A$, peak $-2.372$ at $F$, falling linearly to 0 at $E$.
- **BC:** compression, peak $-1.581$ under $G$; $-0.791$ under $F$ and $H$.
- **BG:** compression, a triangle between $A$ and $G$ with peak $-1.581$ at $F$; zero for load beyond $G$.

## Check yourself

The answer's key points as multiple-choice questions, with the correct option and why.

1. Why is F_AB = -3.162 R_A?
   A. AB is a tension member
   B. Joint A vertical equilibrium: F_AB sin(alpha) = -R_A with sin(alpha) = 0.316
   C. AB is horizontal
   D. Moments about G
   Answer: B. At joint A the only vertical forces are R_A and the vertical component of AB, so F_AB = -R_A/0.316 = -3.162 R_A (compression). (Key point: Member AB from joint A)

2. What is the peak ordinate of the BC influence line, under G (x = 30 m)?
   A. -3.162
   B. -0.791
   C. -2.372
   D. -1.581
   Answer: D. At G, R_A = 0.5, so F_BC = -3.162 x 0.5 = -1.581 (compression). (Key point: BC peak ordinate)

3. Why is F_BG = 0 for a load to the right of G?
   A. Moments about A: the left part has only R_A which passes through A, so BG carries nothing
   B. Because BG is a zero-force member by joint rule always
   C. Because the load goes directly to E
   D. Because BG is vertical
   Answer: A. BC and FG meet at A, the moment centre. For a load right of G the left part has only R_A, whose moment about A is zero, so F_BG = 0. (Key point: BG moment centre)

4. What is the AB ordinate under F (x = 15 m)?
   A. -1.581
   B. -2.372
   C. -0.791
   D. -3.162
   Answer: B. R_A at F = 45/60 = 0.75, so F_AB = -3.162 x 0.75 = -2.372. (Key point: Ordinate of AB)

## Related in Theory of Structures I

- [Truss ILDs for BC and BG; max force in BC](https://www.bctengineer.com/question.md?key=semester_4%2Ftheory_of_structures_i%3Atruss-ild-bc-bg-live-load-8m) — Theory of Structures I, chapter 5
- [Truss ILDs for six members, load on bottom chord](https://www.bctengineer.com/question.md?key=semester_4%2Ftheory_of_structures_i%3Atruss-ild-six-members-bottom) — Theory of Structures I, chapter 5
- [Truss ILDs for BC, CH, HG, bottom chord](https://www.bctengineer.com/question.md?key=semester_4%2Ftheory_of_structures_i%3Atruss-ild-bc-ch-hg-bottom) — Theory of Structures I, chapter 5
- [Truss ILDs for bc, hg, df, upper chord](https://www.bctengineer.com/question.md?key=semester_4%2Ftheory_of_structures_i%3Atruss-ild-bc-hg-df-upper-chord) — Theory of Structures I, chapter 5
- [Truss ILDs for LC, LK, LD, lower chord](https://www.bctengineer.com/question.md?key=semester_4%2Ftheory_of_structures_i%3Atruss-ild-lc-lk-ld-lower) — Theory of Structures I, chapter 5, asked 2×
- [Truss ILDs for FG and BG](https://www.bctengineer.com/question.md?key=semester_4%2Ftheory_of_structures_i%3Atruss-ild-fg-bg-2076b) — Theory of Structures I, chapter 5

## Related in other subjects

- [Truss indeterminacy; forces in BC, BG, HG, GD](https://www.bctengineer.com/question.md?key=semester_1%2Fapplied_mechanics%3Atruss-indeterminacy-bc-bg-hg-gd) — Applied Mechanics, chapter 7
- [Forces in all members of truss with 10.8 kN loads](https://www.bctengineer.com/question.md?key=semester_1%2Fapplied_mechanics%3Atruss-forces-10-8kn-d-support) — Applied Mechanics, chapter 7
- [Truss bar forces BG, HC, CF](https://www.bctengineer.com/question.md?key=semester_5%2Ftheory_of_structures_ii%3Atruss-bar-forces-bg-hc-cf) — Theory of Structures II, chapter 2
- [Truss member forces BC, BD, BE, DE, DG, EG](https://www.bctengineer.com/question.md?key=semester_1%2Fapplied_mechanics%3Atruss-bc-bd-be-de-dg-eg-48kn) — Applied Mechanics, chapter 7
