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Pa
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kPa
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MPa
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GPa
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psi
Enter values to see results
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Pa
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kPa
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MPa
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GPa
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psi
Stress is one of the most fundamental concepts in mechanics and materials science — it quantifies the internal force intensity within a material caused by external loads. Understanding stress is essential for ensuring structural integrity, selecting appropriate materials, and preventing mechanical failure. This calculator computes normal stress from applied force and cross-sectional area, converting results to Pa, kPa, MPa, GPa, and psi.
Normal stress (also called engineering stress or nominal stress) is defined as the force acting perpendicular to a surface divided by the area of that surface:
$$\sigma = \frac{F}{A}$$
where:
The SI unit of stress is the Pascal (Pa), which equals one Newton per square meter. Because the Pascal is a very small unit for engineering materials, stress is commonly expressed in:
There are two fundamental types of normal stress:
Tensile stress occurs when forces pull the material apart (positive σ by convention). Examples include cables, ropes, and the bottom flange of a simply supported beam.
Compressive stress occurs when forces push the material together (negative σ by convention). Examples include columns, foundations, and the top flange of a simply supported beam.
The concept extends to more complex loading scenarios. Shear stress (τ = F/A) acts parallel to the surface. In general three-dimensional loading, the complete state of stress at a point is described by the Cauchy stress tensor — a 3×3 symmetric matrix with six independent components:
$$\boldsymbol{\sigma} = \begin{bmatrix} \sigma_{xx} & \tau_{xy} & \tau_{xz} \\ \tau_{yx} & \sigma_{yy} & \tau_{yz} \\ \tau_{zx} & \tau_{zy} & \sigma_{zz} \end{bmatrix}$$
Engineers compare calculated stress to a material's yield strength (σ_y) and ultimate tensile strength (σ_u) to assess safety. The factor of safety is FoS = σ_y / σ_applied. Typical design requires FoS of 1.5–4 depending on the application, consequences of failure, and load uncertainty.
The calculated stress should be compared against material strength limits. For structural steel (σ_y ≈ 250 MPa), stress below ~160 MPa provides a factor of safety around 1.5. If your stress exceeds the material's yield strength, plastic deformation will occur; if it exceeds the ultimate strength, fracture is imminent. Note this calculator assumes uniform stress distribution — stress concentrations near holes, notches, and fillets can multiply local stresses by factors of 2–5 or more.
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A steel cable with 200 mm² cross-section carrying 50 kN: σ = 50,000 N / (200 × 10⁻⁶ m²) = 250 MPa. This equals the yield strength of mild steel — the cable is at its elastic limit.
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A 300×300 mm concrete column supporting 500 kN: σ = 500,000 / 0.09 = 5.56 MPa. Typical concrete compressive strength is 20–40 MPa, giving a factor of safety of 3.6–7.2.
Both have units of force per area (Pa), but they describe different things. Pressure is an external load applied to a surface (always compressive, acts equally in all directions in fluids). Stress is the internal response within a material to applied loads — it can be tensile, compressive, or shear, and varies with direction and location within the body.
Engineering stress uses the original cross-sectional area: σ_eng = F/A₀. True stress uses the current (deformed) area: σ_true = F/A_current. They are nearly identical for small strains (<5%), but diverge significantly during plastic deformation. True stress accounts for necking and is always higher than engineering stress during tension: σ_true = σ_eng(1 + ε_eng).
When stress exceeds the yield strength (σ_y), the material enters plastic deformation — it will not return to its original shape when unloaded. Continued loading increases stress toward the ultimate tensile strength (σ_u), where necking begins. Beyond σ_u, the material fractures. Ductile materials like steel show significant plastic deformation before fracture; brittle materials like glass fracture with little warning.
Stress concentrations occur at geometric discontinuities — holes, notches, sharp corners, and cross-section changes. The local stress at these points is K_t × σ_nominal, where K_t is the stress concentration factor (typically 2–5). This calculator gives nominal (average) stress. For critical designs, multiply by K_t from handbooks or FEA analysis to get the actual peak stress.
For bending stress in a beam, use the flexure formula: σ = My/I, where M is the bending moment, y is the distance from the neutral axis, and I is the moment of inertia. Maximum bending stress occurs at the outer fibers. For combined axial and bending: σ = F/A ± My/I. Shear stress in a beam: τ = VQ/(Ib), where V is shear force, Q is the first moment of area, and b is width.
Use MPa for most structural and mechanical engineering (material strengths are typically quoted in MPa). Use kPa for soil mechanics and low-load applications. Use GPa for elastic moduli. Use psi (or ksi = 1000 psi) in US customary practice. Always ensure force and area units are consistent before dividing — this calculator handles the unit conversions automatically.
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