Stress Strain Calculator
Plan your materials project with our free stress strain calculator. Get precise measurements, material lists, and budgets.
Stress Strain Calculator
Calculator
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Formula: σ = F/A | ε = ΔL/L₀ | E = σ/ε | FoS = σ_yield / σ_working
Worked example — σ = 199.90 MPa | ε = 0.1% | E = 199.9 GPa | FoS = 1.251
Formula
σ = F/A | ε = ΔL/L₀ | E = σ/ε | FoS = σ_yield / σ_working
Stress equals force divided by cross-sectional area. Strain equals the change in length divided by original length. Young's modulus (elastic modulus) is the ratio of stress to strain in the linear elastic region. Factor of safety is yield strength divided by working stress.
Worked Examples
Example 1: Steel Rod Under Tension
Problem:A steel rod (10mm diameter, 500mm long) stretches 0.50mm under a 15,700N tensile load. Calculate stress, strain, Young's modulus, and FoS (yield = 250 MPa).
Solution:Area = π(5mm)² = 78.54 mm² Stress σ = 15700 / 78.54e-6 = 199.90 MPa Strain ε = 0.50/500 = 0.001 (0.1%) Young's Modulus E = 199.90/0.001 = 199,900 MPa ≈ 199.9 GPa (Steel) FoS = 250/199.90 = 1.251
Result:σ = 199.90 MPa | ε = 0.1% | E = 199.9 GPa | FoS = 1.251
Example 2: Aluminum Column Under Compression
Problem:An aluminum column (25mm × 25mm cross-section, 300mm long) shortens by 0.312mm under 44,850N compressive load. Yield strength = 276 MPa.
Solution:Area = 25 × 25 = 625 mm² Stress σ = 44850 / 625e-6 = 71.76 MPa Strain ε = 0.312/300 = 0.00104 (0.104%) Young's Modulus E = 71.76/0.00104 = 69,000 MPa ≈ 69 GPa ✓ (Aluminum) FoS = 276/71.76 = 3.85
Result:σ = 71.8 MPa | ε = 0.104% | E = 69 GPa | FoS = 3.85
Frequently Asked Questions
What is stress in engineering?
Engineering stress (sigma, σ) is the internal force per unit area within a material, caused by externally applied forces. It is calculated as σ = F/A, where F is the applied force (Newtons) and A is the cross-sectional area (m²). Stress is measured in Pascals (Pa) or commonly in Megapascals (MPa) for engineering materials. There are three main types: tensile stress (pulling apart), compressive stress (pushing together), and shear stress (sliding). Understanding stress is fundamental to structural design — every component must be designed so that the working stress remains safely below the material's yield strength.
What is strain?
Strain (epsilon, ε) is the measure of deformation representing the displacement between particles in a material. Engineering strain is calculated as ε = ΔL/L₀, where ΔL is the change in length and L₀ is the original length. Strain is dimensionless (no units) and is often expressed as a percentage or in microstrain (με = strain × 10⁶). Positive strain indicates elongation (tensile), negative strain indicates compression. Typical elastic strains in metals are very small, on the order of 0.001 to 0.01 (0.1% to 1%). Beyond the elastic limit, permanent plastic deformation occurs.
What is Young's modulus?
Young's modulus (E), also called the modulus of elasticity, is the ratio of stress to strain in the elastic (linear) region: E = σ/ε. It measures a material's stiffness — its resistance to elastic deformation. Units are the same as stress (Pa or GPa). Common values: Steel = 200 GPa, Aluminum = 69 GPa, Copper = 117 GPa, Titanium = 116 GPa, Concrete = 30 GPa, Wood = 12 GPa, Rubber = 0.01-0.1 GPa. A higher Young's modulus means a stiffer material. It is an intrinsic material property independent of geometry.
What is factor of safety?
Factor of Safety (FoS) is the ratio of a material's strength to the actual applied stress: FoS = Yield Strength / Working Stress. It provides a margin against uncertainty in loading, material properties, and analysis methods. Common FoS values: Static loads with well-known materials = 1.5-2.0. Dynamic/fatigue loads = 2.0-3.0. Impact or shock loads = 3.0-5.0. Life-critical applications (bridges, aircraft) = 4.0-8.0. Unknown loads or materials = 5.0-10.0. A FoS of 1.0 means the component is at the verge of yielding, and values below 1.0 indicate failure.
What is the difference between stress and pressure?
While both stress and pressure are force per unit area (Pa), they differ fundamentally. Pressure is an external force applied to a surface, is always compressive (pushes inward), is a scalar quantity (equal in all directions in a fluid), and acts on the boundary of an object. Stress is an internal reaction within the material, can be tensile, compressive, or shear, is a tensor quantity (varies with direction and plane), and exists throughout the volume of the material. In engineering, pressure refers to fluid/gas forces on surfaces, while stress refers to the material's internal response to all applied loads.
What is the difference between engineering stress and true stress?
Engineering stress divides the load by the original cross-sectional area, while true stress divides it by the instantaneous area that shrinks as the specimen elongates. Up to the onset of necking and assuming constant volume, the two are linked by true stress = engineering stress times (1 + engineering strain), and true strain = ln(1 + engineering strain). The engineering curve therefore appears to drop after the ultimate tensile point, whereas the true curve keeps rising. Stress Strain Calculator reports engineering values, which is the convention for design codes and material data sheets.
How is yield strength determined when a material has no sharp yield point?
Mild steel shows a distinct upper and lower yield point, but aluminium, copper and most alloys transition gradually from elastic to plastic behaviour. For those, the 0.2 percent offset method is used: a line is drawn parallel to the initial elastic slope but shifted 0.002 in strain, and its intersection with the stress-strain curve defines the offset yield strength. That is the number quoted on data sheets and the value you should enter here for a factor-of-safety check on a non-ferrous alloy.
What is Poisson's ratio and how does it relate to Young's modulus?
Poisson's ratio is the negative of the lateral strain divided by the axial strain, describing how much a bar thins as it stretches. Most metals fall between about 0.25 and 0.35, with steel near 0.30 and aluminium near 0.33, while elastomers approach 0.5 because they deform at nearly constant volume. For an isotropic material it links the elastic constants through the shear modulus relationship G equals E divided by twice the quantity one plus Poisson's ratio, so knowing E and Poisson's ratio fixes G.
Should the factor of safety be based on yield strength or ultimate tensile strength?
For ductile metals the usual design limit is yield strength, because permanent set makes a part unserviceable long before it separates, and Stress Strain Calculator's factor of safety uses that basis. Brittle materials such as grey cast iron, ceramics and concrete in tension have little plastic reserve and no meaningful yield point, so their allowable stress is normally referenced to ultimate strength with a larger margin. Mixing the two bases is a common error that can make a design look far safer than it is.
Why does the nominal stress from force divided by area understate the real peak stress?
The F/A calculation gives the average stress across the section, but any geometric discontinuity redistributes the load and raises the local value. The classic elastic result for a small circular hole in a wide plate under uniaxial tension is a stress concentration factor of three at the hole edge, and sharp fillets, notches and keyways produce comparable multipliers. Peak stress equals the concentration factor times the nominal stress, so for fatigue or brittle-material design the nominal figure must be multiplied by the appropriate factor.
References
Background & Theory
History
Reviewed for accuracy by Daniel Agrici, Founder & Lead Developer · Editorial policy
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