Skip to main content
Speclore

Weight Beam Stress Strain

Reference data and engineering information about weight beam stress strain for material properties applications.

weightbeamstressstrainCalculator

Overview

Engineering reference data for Weight Beam Stress Strain in material science and properties.

Key Formulas

Stress

σ=FA\sigma = \frac{F}{A}

Force per unit area.

Strain

ε=ΔLL0\varepsilon = \frac{\Delta L}{L_0}

Change in length per original length.

Hooke's Law

σ=Eε\sigma = E \varepsilon

Stress proportional to strain in elastic region.

Thermal Expansion

ΔL=αL0ΔT\Delta L = \alpha L_0 \Delta T

Length change due to temperature.

Variables

SymbolDescriptionUnit
σ\sigmaStressPa
ε\varepsilonStrain
EEYoung's modulusPa
α\alphaThermal expansion coefficient1/°C
ΔT\Delta TTemperature change°C

Example: Stress and Axial Deformation in a Vertical Steel Rod

Consider a 45 m long steel rod with density ρ=7280kg/m3\rho = 7280 \, \text{kg/m}^3 and cross-sectional area A=0.1m2A = 0.1 \, \text{m}^2. The modulus of elasticity for steel is E=200GPa=200×109N/m2E = 200 \, \text{GPa} = 200 \times 10^9 \, \text{N/m}^2.

Maximum Axial Force at x=0mx = 0 \, \text{m}: Using Fx=ρgA(Lx)F_x = \rho g A (L - x), Fx=0=(7280kg/m3)(9.81m/s2)(0.1m2)(45m0m)=321376N321kNF_{x=0} = (7280 \, \text{kg/m}^3)(9.81 \, \text{m/s}^2)(0.1 \, \text{m}^2)(45 \, \text{m} - 0 \, \text{m}) = 321376 \, \text{N} \approx 321 \, \text{kN}

Maximum Axial Stress at x=0mx = 0 \, \text{m}: From σx=ρg(Lx)\sigma_x = \rho g (L - x), σx=0=(7280kg/m3)(9.81m/s2)(45m)=3213756Pa3.2MPa\sigma_{x=0} = (7280 \, \text{kg/m}^3)(9.81 \, \text{m/s}^2)(45 \, \text{m}) = 3213756 \, \text{Pa} \approx 3.2 \, \text{MPa}

Axial Deformation at x=45mx = 45 \, \text{m}: Using dx=ρgx(2Lx)2Ed_x = \frac{\rho g x (2L - x)}{2E}, dx=45=(7280kg/m3)(9.81m/s2)(45m)22×200×109N/m2=0.00036m=0.4mmd_{x=45} = \frac{(7280 \, \text{kg/m}^3)(9.81 \, \text{m/s}^2)(45 \, \text{m})^2}{2 \times 200 \times 10^9 \, \text{N/m}^2} = 0.00036 \, \text{m} = 0.4 \, \text{mm}

Key Observations for Vertical Beams Under Self-Weight

  • Stress Independence from Cross-Section: The axial stress σx=ρg(Lx)\sigma_x = \rho g (L - x) is independent of the cross-sectional area AA. This simplifies analysis, as stress depends only on material density, gravity, and beam length.
  • Maximum Stress Location: Maximum axial stress occurs at the top of the beam (x=0x = 0), where σmax=ρgL\sigma_{\text{max}} = \rho g L. This is critical for design, as it determines the highest load point.
  • Zero Stress at Free End: At the free end (x=Lx = L), the axial stress is zero, reflecting no load from below.
  • Deformation Profile: The axial deformation dx=ρgx(2Lx)2Ed_x = \frac{\rho g x (2L - x)}{2E} follows a quadratic distribution, with maximum deformation at the free end (x=Lx = L), calculated as dL=ρgL22Ed_{L} = \frac{\rho g L^2}{2E}.

References