---
title: "Simply supported beam with two elements"
subject: "Finite Element Method"
chapter: 3
key: "semester_8/finite_element_method:simply-supported-beam-two-elements"
source: https://www.bctengineer.com/q/semester_8/finite_element_method/simply-supported-beam-two-elements
site: BCT Engineering
---

# Simply supported beam with two elements

Finite Element Method · Chapter 3: Direct Stiffness Method: Discrete Finite Elements

- Asked in: year not given, 8 marks
- Video: [Nodal Force Vector for Beam with UDL and Point Load | FEA | Combined  UDL & Point Load using FEM](https://www.youtube.com/watch?v=WQMCEG8g7BA) — Mahesh Gadwantikar
- Answer checked by Claude Opus 5.5 (high effort) on 2026-10-14
- Page: https://www.bctengineer.com/q/semester_8/finite_element_method/simply-supported-beam-two-elements
- Whole chapter: https://www.bctengineer.com/md/semester_8/finite_element_method/chapter-3

## Question

A simply supported beam of span 4 m carries a point load of 10 kN at mid-span. $E = 200$ GPa and $I = 8\times10^6\ \text{mm}^4$. Model the beam with two equal beam elements. Find the deflection at mid-span, the rotations at the supports and the support reactions, and compare the deflection with the exact value.

## Short answer

With two 2 m beam elements (EI=1.6×10⁶ N·m²), symmetry gives θ₂=0 and θ₃=−θ₁. Solving yields mid-span deflection 8.33 mm downward, support rotations ±6.25×10⁻³ rad. Reactions are 5 kN each. Results match the exact solution PL³/(48EI) exactly because the cubic element is exact for nodal loads.

## Answer

#### Data

$EI = 200\times10^9 \times 8\times10^{-6} = 1.6\times10^6\ \text{N m}^2$, $L_e = 2$ m for each element.

$\dfrac{EI}{L_e^3} = \dfrac{1.6\times10^6}{8} = 2\times10^5$ N/m.

Nodes: 1 (left support), 2 (mid-span), 3 (right support). Degrees of freedom: $(v_1, \theta_1, v_2, \theta_2, v_3, \theta_3)$. Boundary conditions: $v_1 = v_3 = 0$.

```text
   ^              10 kN
   |               |
   o======= (1) ===o======= (2) ===o
  1                2                3
  |<------ 2 m ---->|<------ 2 m -->|
```

#### Element matrix (each element)

With $L_e = 2$:
$$
[k] = 2\times10^5\begin{bmatrix} 12 & 12 & -12 & 12 \\ 12 & 16 & -12 & 8 \\ -12 & -12 & 12 & -12 \\ 12 & 8 & -12 & 16 \end{bmatrix}
$$

#### Reduced system

Free DOFs: $\theta_1, v_2, \theta_2, \theta_3$. By symmetry about mid-span, $\theta_2 = 0$ and $\theta_3 = -\theta_1$.

Row for $\theta_1$ (element 1, second row), with $v_1 = 0$, $\theta_2 = 0$:
$$
2\times10^5\,(16\theta_1 - 12v_2) = 0
$$

Row for $v_2$ (sum of element 1 third row and element 2 first row), with $v_1 = v_3 = 0$, $\theta_2 = 0$, $\theta_3 = -\theta_1$:
$$
2\times10^5\,(-12\theta_1 + 24v_2 + 12\theta_3) = 2\times10^5\,(-24\theta_1 + 24v_2) = -10\,000
$$

So $\theta_1 = 0.75v_2$, and $-18v_2 + 24v_2 = -0.05$ gives
$$
v_2 = -0.008333\ \text{m},\qquad \theta_1 = -0.00625\ \text{rad}
$$

#### Reactions

$R_1 = 2\times10^5(12v_1 + 12\theta_1 - 12v_2 + 12\theta_2) = 2.4\times10^6(-0.00625 + 0.008333) = 5000$ N, and by symmetry $R_3 = 5000$ N.

#### Comparison

Exact: $v_{max} = \dfrac{PL^3}{48EI} = \dfrac{10\,000(4)^3}{48(1.6\times10^6)} = 8.333$ mm; exact support rotation $\dfrac{PL^2}{16EI} = 6.25\times10^{-3}$ rad. The FE results match exactly because the cubic element is exact for a load applied at a node.

**Answer:** mid-span deflection = 8.33 mm downward; support rotations = 6.25 $\times10^{-3}$ rad (left clockwise, right anticlockwise); reactions = 5 kN each; the FE result equals the exact value.

## Check yourself

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

1. What is EI/Le^3 for each element (EI = 1.6 x 10^6 N m^2, Le = 2 m)?
   A. 2 x 10^5 N/m
   B. 8 x 10^5 N/m
   C. 1.6 x 10^6 N/m
   D. 4 x 10^5 N/m
   Answer: A. EI/Le^3 = 1.6 x 10^6 / 8 = 2 x 10^5 N/m. (Key point: Element data)

2. Which relation follows from symmetry about mid-span?
   A. v2 = 0
   B. theta2 = 0 and theta3 = -theta1
   C. theta1 = theta3
   D. theta2 = theta1
   Answer: B. At mid-span the slope is zero by symmetry, and the end rotations are equal in size but opposite in sense. (Key point: Symmetry)

3. What is the mid-span deflection?
   A. 0.833 mm
   B. 83.3 mm
   C. 8.33 mm downward
   D. 20 mm
   Answer: C. v2 = -0.008333 m, so the mid-span deflection is 8.33 mm downward. (Key point: Deflection)

4. What are the support reactions?
   A. 10 kN each
   B. 2.5 kN each
   C. 10 kN and 0
   D. 5 kN each
   Answer: D. By symmetry each support carries half of the 10 kN load. (Key point: Reactions)

## Related in Finite Element Method

- [Ritz solution of beam under uniform load](https://www.bctengineer.com/question.md?key=semester_8%2Ffinite_element_method%3Aritz-simply-supported-beam) — Finite Element Method, chapter 4
- [Tapered bar analysis using two elements](https://www.bctengineer.com/question.md?key=semester_8%2Ffinite_element_method%3Atapered-bar-two-elements) — Finite Element Method, chapter 5
- [Ritz method for bar with distributed load](https://www.bctengineer.com/question.md?key=semester_8%2Ffinite_element_method%3Aritz-bar-quadratic-trial) — Finite Element Method, chapter 4
- [Two-bar plane truss displacement and member forces](https://www.bctengineer.com/question.md?key=semester_8%2Ffinite_element_method%3Atwo-bar-truss-member-forces) — Finite Element Method, chapter 3

## Related in other subjects

- [Mid-span deflection of beam, 10 kN load](https://www.bctengineer.com/question.md?key=semester_3%2Fstrength_of_materials%3Ass-beam-deflection-mid-span-4m) — Strength of Materials, chapter 7
- [Beam reactions and mid-span deflection (2EI)](https://www.bctengineer.com/question.md?key=semester_8%2Fcomputational_techniques_in_civil_engineering%3Abeam-support-reactions-midspan-k8) — Computational Techniques in Civil Engineering, chapter 4, asked 2×
- [Beam deflection at B, rotations (2 elements)](https://www.bctengineer.com/question.md?key=semester_8%2Fcomputational_techniques_in_civil_engineering%3Abeam-two-elements-b-c) — Computational Techniques in Civil Engineering, chapter 4
- [Simply supported beam 6 m, 60 kN/m](https://www.bctengineer.com/question.md?key=semester_6%2Fdesign_of_steel_and_timber_structure%3Abeam-6m-60knm-udl) — Design of Steel and Timber Structure, chapter 7
