Structural Beam Testing Loading Frame
Rigid steel reaction frame with hydraulic screw jack applying central vertical point loads to 25 kN.
Verify the Euler–Bernoulli beam flexure theory, measure midspan elastic deflection (δ) under central point loading across span L, and determine the flexural rigidity (EI) of a structural steel beam. Explore interactive structural mechanics, materials simulation, and civil engineering telemetry.
Ready to sample with Load P = 8.0 kN.
Adjust Load P, 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 (2.0 to 14.0 kN). Structural steel beam of span L = 1200 mm, moment of inertia I = 4.235 x 10^5 mm^4, E = 200 GPa. Theoretical compliance slope: L^3 / (48 E I) = 1200^3 / (48 · 200,000 · 423,500) = 1.728 x 10^9 / 4.0656 x 10^12 = 0.4250 mm/kN.
Rigid steel reaction frame with hydraulic screw jack applying central vertical point loads to 25 kN.
Provides true simply supported boundary conditions (one pinned knife-edge, one sliding roller).
Measures beam midspan vertical deflection with 0.001 mm resolution and 25 mm travel.
Measures applied concentrated central load P with 0.01 kN precision.
Structural steel rectangular/I-beam with machined straight edges and known cross-sectional geometry.
Measures span length L, beam width b, and beam depth d to 0.05 mm precision.
Verify the Euler–Bernoulli beam flexure theory, measure midspan elastic deflection (δ) under central point loading across span L, and determine the flexural rigidity (EI) of a structural steel beam. Standardized parameter settings: 2.0, 4.0, 6.0, 8.0, 10.0, 12.0, 14.0 kN.
Measure beam cross-sectional width b and depth d at three stations using callipers to 0.05 mm; compute moment of inertia I = b d^3 / 12.
Position pinned support and roller support on the reaction bed; set clear span L = 1200.0 mm using precision rule; place beam centrally on supports.
Mount loading knife-edge saddle at exact midspan (x = 600 mm); position digital dial indicator directly beneath midspan bottom flange; zero the indicator.
Apply a gentle seating load of 1.0 kN to settle knife-edges; release load completely and re-zero dial gauge.
Apply central point load incrementally in steps of 2.0 kN through 2.0, 4.0, 6.0, 8.0, 10.0, 12.0, and 14.0 kN; record steady midspan deflection δ at each plateau.
Decrement load in reverse steps back to zero; verify that residual plastic deflection is zero (< 0.02 mm) to confirm true elastic behavior.
Points are your recorded observations. The solid regression line validates Beam Elastic Deflection mathematical scaling.
| # | Central Point Load P (kN) | Midspan Deflection δ (mm) | Central point load P (kN) | Midspan deflection δ (mm) | Remove |
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No readings yet. Execute a civil engineering trial and record it.
In structural civil engineering, the serviceability limit state (deflection control) is just as critical as the ultimate strength limit state. Excessive beam deflections cause unsightly sagging, crack plaster and brittle architectural finishes, jam doors and operable windows, and induce alarming vibrations under human foot traffic. Classical Euler–Bernoulli beam theory dictates that the elastic deflection curve v(x) of a prismatic, homogeneous beam of flexural rigidity EI obeys the fundamental second-order differential equation d^2v/dx^2 = M(x) / (EI), where M(x) is internal bending moment. For a simply supported beam of span L subjected to a concentrated central point load P at midspan (x = L/2), double integration with boundary conditions (zero deflection at supports x = 0 and x = L) yields the famous midspan deflection expression: δ = P L^3 / (48 E I). Measuring midspan deflection δ as a function of load P produces a linear elastic compliance slope C = δ / P = L^3 / (48 E I), from which the experimental flexural rigidity EI and Young's modulus E can be deduced. In this laboratory, a structural steel I-beam is loaded across loads from 2 to 14 kN using digital dial indicators to verify beam flexure theory and evaluate flexural compliance.
Structural steel beam of span L = 1200 mm, moment of inertia I = 4.235 x 10^5 mm^4, E = 200 GPa. Theoretical compliance slope: L^3 / (48 E I) = 1200^3 / (48 · 200,000 · 423,500) = 1.728 x 10^9 / 4.0656 x 10^12 = 0.4250 mm/kN.