Estimate deformation and identify a likely failure mode.
2 core ideas2 source trails3 recall prompts
Load path01—04
Force meets areaNominal stress changes when the same load is carried by a different section.Mechanics · Modules
Build the idea
An original introduction, worked example and practice, followed by a curated reading sequence. The external courses supply deeper teaching and problem sets.
Scope and safety
This guide is an orientation, not a complete university module. Practical work needs suitable facilities, safety review and supervision.
Equilibrium finds loads. Mechanics of materials connects those loads to stress, strain and deformation under stated material and geometry assumptions.
Module lens
Load meets section area
Nominal stress is a first model of how an axial load is distributed over a section.
Core relationshipσ = F / A
Track
Pa · N · mm²
Ask yourself
What changes if the area doubles?
Original Lilerno schematic · conceptual, not to scale
01
Distinguish average stress from local stress
For a straight axially loaded member, average normal stress is force divided by cross-sectional area. Holes, notches and load introduction can produce local concentrations. Nominal stress alone does not predict every failure mode.
02
Elastic is a limited regime
In one-dimensional linear elasticity, stress equals Young's modulus times strain. Strain is extension divided by original length. Check units and the validity of small deformation and material assumptions before extending the formula to bending or buckling.
Load path01—04
Force meets areaNominal stress changes when the same load is carried by a different section.
See the relationship
Change one quantity, watch the graph respond, then explain the result in your own words.
Predict → change → explain
Load, area and axial stress
Double the area while preserving force. What happens to nominal stress?
1Axial load F
2Cross-section A
3Nominal stress F/A
4Check material + geometry
Average stress
10 MPa
Area
100 mm²
Uniform axial bar with fixed left boundary and tensile end load. Geometry and displacement are schematic; use the numerical results for magnitude.
Nominal stress
Chosen section
Axes: Area (mm²) → Stress (MPa). Bounds may rescale when inputs change.
σ = 10 MPa. 1 N/mm² = 1 MPa. This is not a load rating.
Model assumptions and limits
Straight uniform axial bar; average stress F/A. No stress concentration, buckling, fatigue or allowable strength is modelled.
Original Lilerno illustration. Inputs are illustrative; this is not experimental evidence or a design rating.
Inspect the plotted values
Area (mm²) and Stress (MPa); values rounded to four significant figures.
Series
Area (mm²)
Stress (MPa)
Nominal stress
20
50
Nominal stress
22.25
44.94
Nominal stress
24.5
40.82
Nominal stress
26.75
37.38
Nominal stress
29
34.48
Nominal stress
31.25
32
Nominal stress
33.5
29.85
Nominal stress
35.75
27.97
Nominal stress
38
26.32
Nominal stress
40.25
24.84
Nominal stress
42.5
23.53
Nominal stress
44.75
22.35
Nominal stress
47
21.28
Nominal stress
49.25
20.3
Nominal stress
51.5
19.42
Nominal stress
53.75
18.6
Nominal stress
56
17.86
Nominal stress
58.25
17.17
Nominal stress
60.5
16.53
Nominal stress
62.75
15.94
Nominal stress
65
15.38
Nominal stress
67.25
14.87
Nominal stress
69.5
14.39
Nominal stress
71.75
13.94
Nominal stress
74
13.51
Nominal stress
76.25
13.11
Nominal stress
78.5
12.74
Nominal stress
80.75
12.38
Nominal stress
83
12.05
Nominal stress
85.25
11.73
Nominal stress
87.5
11.43
Nominal stress
89.75
11.14
Nominal stress
92
10.87
Nominal stress
94.25
10.61
Nominal stress
96.5
10.36
Nominal stress
98.75
10.13
Nominal stress
101
9.901
Nominal stress
103.3
9.685
Nominal stress
105.5
9.479
Nominal stress
107.8
9.281
Nominal stress
110
9.091
Nominal stress
112.3
8.909
Nominal stress
114.5
8.734
Nominal stress
116.8
8.565
Nominal stress
119
8.403
Nominal stress
121.3
8.247
Nominal stress
123.5
8.097
Nominal stress
125.8
7.952
Nominal stress
128
7.813
Nominal stress
130.3
7.678
Nominal stress
132.5
7.547
Nominal stress
134.8
7.421
Nominal stress
137
7.299
Nominal stress
139.3
7.181
Nominal stress
141.5
7.067
Nominal stress
143.8
6.957
Nominal stress
146
6.849
Nominal stress
148.3
6.745
Nominal stress
150.5
6.645
Nominal stress
152.8
6.547
Nominal stress
155
6.452
Nominal stress
157.3
6.359
Nominal stress
159.5
6.27
Nominal stress
161.8
6.182
Nominal stress
164
6.098
Nominal stress
166.3
6.015
Nominal stress
168.5
5.935
Nominal stress
170.8
5.857
Nominal stress
173
5.78
Nominal stress
175.3
5.706
Nominal stress
177.5
5.634
Nominal stress
179.8
5.563
Nominal stress
182
5.495
Nominal stress
184.3
5.427
Nominal stress
186.5
5.362
Nominal stress
188.8
5.298
Nominal stress
191
5.236
Nominal stress
193.3
5.175
Nominal stress
195.5
5.115
Nominal stress
197.8
5.057
Nominal stress
200
5
Chosen section
100
10
Your progress0 reviews
Ready to move on?
Save your place when you finish reading.
Self-reported recall, not an assessment of mastery.
Original Lilerno example
An ideal axial bar carries 1,000 N through an area of 100 mm². Find average stress.
01
Use σ = F/A.
02
1,000/100 = 10 N/mm².
03
1 N/mm² = 1 MPa, so average stress is 10 MPa.
σ=AF=10N/mm2=10MPa
No allowable stress or material strength was supplied; safety cannot be inferred.
Load path01—04
Force meets areaNominal stress changes when the same load is carried by a different section.
Test the model
Open learning, traceable sources
Work in this order. These links open the publisher’s material; free access does not always permit republication.
Identify the internal resultants before evaluating stress.
Recall, then record
Close the explanation and answer these in your own words. Return tomorrow, then again later in the week.
01
Is this stress local or average?
02
Which constitutive law are you using?
03
What other failure modes are possible?
Engineering notebook
Make a units-checked axial stress and deformation calculation with explicitly assumed geometry and modulus. Do not use it as a fabrication specification.
Your study record
Self-reported tasks, not an assessment of mastery or university credit. Reading a page does not complete a chapter.
Loading local record…
Loading progress…
Open learning, traceable sources
Read further
Checked 2026-09-06
Original Lilerno lessons and diagrams, supported by these references. Free access does not always permit republication. Links open the publisher’s material.
Engineering Statics: Open and InteractiveDaniel W. Baker and William Haynes+
Forces, free-body diagrams, equilibrium, and structures.
CC BY-NC-SA 4.0; reference only. Embedded tools have separate terms.