Transmission Circular Polariscope System
Optical bench with monochromatic light source (589 nm sodium vapor), dual linear polarizers, and dual quarter-wave plates.
Determine the elastic stress concentration factor (K_t) and calibrate the photoelastic fringe constant (f_σ) around a circular cutout in a structural tension plate using transmission photoelasticity according to ASTM E1319. Explore interactive structural mechanics, materials simulation, and civil engineering telemetry.
Ready to sample with Stress σ_nom = 15.0 MPa.
Adjust Stress σ_nom, then execute civil engineering measurement.
Civil engineering telemetry is evaluated rigorously using 64-bit IEEE 754 precision. Residuals reflect ordinary least-squares regression across successive observations. Continuous data structures support high-fidelity structural mechanics and geotechnical continuum modeling.
The civil engineering physical models apply within the specified calibrated operational window (5.0 to 30.0 MPa). Polycarbonate model plate (thickness t = 6.0 mm, width w = 60 mm, hole diameter d = 12 mm, d/w = 0.20). Theoretical Kirsch solution K_t = 3.00 (finite-width corrected K_t = 2.45). Linearized model relates fringe order N directly to nominal stress σ_nom with slope 0.2450 fringes/MPa.
Optical bench with monochromatic light source (589 nm sodium vapor), dual linear polarizers, and dual quarter-wave plates.
Applies smooth, uniform uniaxial tensile load to transparent photoelastic specimens with load cell readout.
Precision CNC-machined polycarbonate plate (6.0 mm thickness) with polished central circular hole.
High-resolution monochrome CMOS camera capturing isochromatic fringe patterns and fringe orders.
Null-balance optical quartz wedge measuring fractional fringe orders to 0.01 fringe precision.
Measures plate width, hole diameter, and thickness to 0.01 mm precision.
Determine the elastic stress concentration factor (K_t) and calibrate the photoelastic fringe constant (f_σ) around a circular cutout in a structural tension plate using transmission photoelasticity according to ASTM E1319. Standardized parameter settings: 5.0, 10.0, 15.0, 20.0, 25.0, 30.0 MPa.
Align polarizer, first quarter-wave plate, second quarter-wave plate, and analyzer along the optical axis; verify dark-field condition (complete extinction) under zero load.
Mount polycarbonate specimen in tensile grips; inspect under polariscope at zero load to verify zero residual machining fringes around the hole boundary.
Energize 589 nm sodium light source; focus digital imaging camera onto the horizontal hole boundary equator.
Apply tensile load incrementally to produce nominal stresses σ_nom of 5.0, 10.0, 15.0, 20.0, 25.0, and 30.0 MPa; count isochromatic fringe orders N emerging at the hole boundary.
At each load step, use the Babinet–Soleil compensator to measure exact fringe order N at the hole edge to within 0.02 fringes.
Plot fringe order N versus nominal stress σ_nom; determine response slope; calculate peak boundary stress and compute stress concentration factor K_t.
Points are your recorded observations. The solid regression line validates Photoelastic Stress Concentration mathematical scaling.
| # | Nominal Applied Tensile Stress σ_nom (MPa) | Isochromatic Fringe Order N (fringes) | Nominal tensile stress σ_nom (MPa) | Isochromatic fringe order N (fringes) | Remove |
|---|
No readings yet. Execute a civil engineering trial and record it.
In structural and bridge engineering, holes, cutouts, notches, and re-entrant corners (such as bolt holes, access manholes, and weld copes) disrupt the uniform flow of internal stress trajectories, concentrating stresses into localized peaks several times greater than the nominal average stress. If left unquantified, these localized stress concentrations initiate fatigue microcracks and catastrophic brittle fractures under cyclic traffic loading. Transmission photoelasticity is a whole-field optical experimental stress analysis technique based on the temporary birefringence (photoelastic effect) of transparent amorphous polymers (e.g. polycarbonate or epoxy). When an unstressed polymer is viewed between crossed circular polarizers in a polariscope, light is extinguished; when loaded in tension, principal stresses σ_1 and σ_2 induce temporary refractive index differences proportional to principal stress difference (σ_1 - σ_2). According to the Stress-Optic Law: σ_1 - σ_2 = N · f_σ / t, where N is the isochromatic fringe order, f_σ is the material fringe constant, and t is model thickness. At the free boundary of a circular hole, radial stress is zero (σ_2 = 0), meaning fringe order N directly reveals peak tangential boundary stress σ_1 = K_t · σ_nom. In this laboratory, photoelastic plates with central circular holes are loaded in tension across stress levels from 5 to 30 MPa to evaluate fringe progression and determine the stress concentration factor K_t.
Polycarbonate model plate (thickness t = 6.0 mm, width w = 60 mm, hole diameter d = 12 mm, d/w = 0.20). Theoretical Kirsch solution K_t = 3.00 (finite-width corrected K_t = 2.45). Linearized model relates fringe order N directly to nominal stress σ_nom with slope 0.2450 fringes/MPa.