Separate material modulus from specimen geometry and validity
A material can deform even when its overall translational motion is in equilibrium. For uniform axial tension, stress is force divided by cross-sectional area and strain is extension divided by original length. Stress has pressure units; strain is dimensionless. The Young modulus E is stress/strain within a stated linear regime, not the same quantity as a particular specimen’s spring stiffness.
Learning outcome: Compare areas1,2,4 mm² at 20 N and compare20 with 40 N at 1 mm². Retain SI area, stress, conditional strain and whether the linear model is valid. Explain why a bounded elastic relation does not establish breaking strength.
Starting recap
Declare the axis, angular units, recipient and valid contact or material branch. Distinguish supplied shape factors from independently measured inertia.
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At F=20 N,A=1 mm², the predicted strain is exactly0.001, the stated boundary, and extension 0.0005 m. This is a permitted model endpoint, not a measured material yield point.
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One square millimetre equals:
Experiment
Compare areas1,2,4 mm² at 20 N and compare20 with 40 N at 1 mm². Retain SI area, stress, conditional strain and whether the linear model is valid. Explain why a bounded elastic relation does not establish breaking strength.
Separate material strain from specimen stiffness
Worked teaching model · synthetic values · Original hypothetical linear material E=2e10 Pa, length .5 m, uniform axial tension. Linear response is stipulated only for strain at most .001. Requested states beyond this limit are labeled unsupported; no strength, fracture or safe-load claim. Areas converted from mm² to m².
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Supported small-strain elastic law
Unlike graph quantities rescale independently; read units and values, not screen angles. 1: linear range only (solid). Joined curves show the supplied model, not additional observations.
Equivalent numerical coordinates for Supported small-strain elastic law
linear range only
| strain (ratio) | tensile stress (Pa) |
|---|---|
| 0 | 0 |
| 0.000025 | 500000 |
| 0.00005 | 1000000 |
| 0.000075 | 1500000 |
| 0.0001 | 2000000 |
| 0.000125 | 2500000 |
| 0.00015 | 3000000 |
| 0.000175 | 3500000 |
| 0.0002 | 4000000 |
| 0.000225 | 4500000 |
| 0.00025 | 5000000 |
| 0.000275 | 5500000 |
| 0.0003 | 6000000 |
| 0.000325 | 6500000 |
| 0.00035 | 7000000 |
| 0.000375 | 7500000 |
| 0.0004 | 8000000 |
| 0.000425 | 8500000 |
| 0.00045 | 9000000 |
| 0.000475 | 9500000 |
| 0.0005 | 10000000 |
| 0.000525 | 10500000 |
| 0.00055 | 11000000 |
| 0.000575 | 11500000 |
| 0.0006 | 12000000 |
| 0.000625 | 12500000 |
| 0.00065 | 13000000 |
| 0.000675 | 13500000 |
| 0.0007 | 14000000 |
| 0.000725 | 14500000 |
| 0.00075 | 15000000 |
| 0.000775 | 15500000 |
| 0.0008 | 16000000 |
| 0.000825 | 16500000 |
| 0.00085 | 17000000 |
| 0.000875 | 17500000 |
| 0.0009 | 18000000 |
| 0.000925 | 18500000 |
| 0.00095 | 19000000 |
| 0.000975 | 19500000 |
| 0.001 | 20000000 |
At most 82 representative computed coordinates including endpoints; the plotted curve can use a finer grid. A table of a revealed generator is not independent measurement evidence.
| Quantity | Value | Unit |
|---|---|---|
| Cross-sectional area in SI | 0.000002 | m² |
| Applied tensile stress | 10000000 | Pa |
| Conditional linear strain | 0.0005 | ratio |
| Stipulated linear range valid | 1 | flag |
| Conditional axial stiffness | 80000 | N/m |
| Predicted extension | 0.00025 | m |
| Elastic stored energy | 0.0025 | J |
Stress and strain describe material response; axial stiffness also depends on specimen geometry.
Stress=F/A, strain=DeltaL/L and E=stress/strain, giving DeltaL=FL/(EA) and k=EA/L only within the declared linear range. One mm² is 10⁻⁶ m², not 10⁻³. A smaller area increases stress and compliance at the same force. The .001 limit is a supplied model boundary, not a measured yield or breaking strength.
Predict before inspecting the values. Save contrasting records with assumptions and one alternative explanation. This virtual display does not certify practical measurement technique.
Stress and strain describe material response; axial stiffness also depends on specimen geometry.
Stress=F/A, strain=DeltaL/L and E=stress/strain, giving DeltaL=FL/(EA) and k=EA/L only within the declared linear range. One mm² is 10⁻⁶ m², not 10⁻³. A smaller area increases stress and compliance at the same force. The .001 limit is a supplied model boundary, not a measured yield or breaking strength.
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Why do a material modulus and a specimen spring constant have different units and geometry dependence?
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