Reference data and engineering information about weight beam stress strain for material properties applications.
Engineering reference data for Weight Beam Stress Strain in material science and properties.
σ=AF
Force per unit area.
ε=L0ΔL
Change in length per original length.
σ=Eε
Stress proportional to strain in elastic region.
ΔL=αL0ΔT
Length change due to temperature.
| Symbol |
Description |
Unit |
| σ |
Stress |
Pa |
| ε |
Strain |
— |
| E |
Young's modulus |
Pa |
| α |
Thermal expansion coefficient |
1/°C |
| ΔT |
Temperature change |
°C |
Consider a 45 m long steel rod with density ρ=7280kg/m3 and cross-sectional area A=0.1m2. The modulus of elasticity for steel is E=200GPa=200×109N/m2.
Maximum Axial Force at x=0m:
Using Fx=ρgA(L−x),
Fx=0=(7280kg/m3)(9.81m/s2)(0.1m2)(45m−0m)=321376N≈321kN
Maximum Axial Stress at x=0m:
From σx=ρg(L−x),
σx=0=(7280kg/m3)(9.81m/s2)(45m)=3213756Pa≈3.2MPa
Axial Deformation at x=45m:
Using dx=2Eρgx(2L−x),
dx=45=2×200×109N/m2(7280kg/m3)(9.81m/s2)(45m)2=0.00036m=0.4mm
- Stress Independence from Cross-Section: The axial stress σx=ρg(L−x) is independent of the cross-sectional area A. 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=0), where σmax=ρgL. This is critical for design, as it determines the highest load point.
- Zero Stress at Free End: At the free end (x=L), the axial stress is zero, reflecting no load from below.
- Deformation Profile: The axial deformation dx=2Eρgx(2L−x) follows a quadratic distribution, with maximum deformation at the free end (x=L), calculated as dL=2EρgL2.