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Arche 2 Strength Of Materials Simulations

A collection of interactive 3D visualizations and simulations to help you master concepts in arche 2 strength of materials.

Module 1: Simple Stresses - Examples & Applications

Concept of internal forces, normal stress, shear stress, bearing stress, and allowable stress.

Normal Stress Visualizer

50 kN
50 kN
Area (AA): 314.2 mm²
Calculated Stress (sigma\\sigma)
159.15 MPa
Adjust the force and the radius of the circular cross-section to see how they affect the normal stress. Notice that increasing the area (radius) decreases the stress, while increasing the force increases the stress.

Module 2: Simple Strain and Deformation - Theory & Concepts - Stress Strain States

Axial deformation, strain concepts, Stress-Strain Diagram, Hooke's Law, Poisson's Ratio, and thermal stresses.

Material Behavior States

Explore how different materials deform under stress

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ε = 0.0000
Current Stress0.0 MPa
Current StateElastic Region

Ductile Steel (e.g., Low Carbon Steel)

Exhibits a distinct elastic region, yield point, a plastic plateau, strain hardening, and necking before fracture. Highly ductile and tough.

What is happening now?

Elastic Region

Material deforms reversibly. Stress is directly proportional to strain (Hooke's Law applies). If the load is removed, the material returns exactly to its original shape. The bonds between atoms are stretched but not broken.

Microscopic View

Atoms are stretched uniformly like springs.

Module 2: Simple Strain and Deformation - Theory & Concepts - Strain Deformation

Axial deformation, strain concepts, Stress-Strain Diagram, Hooke's Law, Poisson's Ratio, and thermal stresses.

Axial Deformation & Stress-Strain Curve

L = 2000mm + 0.00mm
0Yield (125 kN)Ultimate (200 kN)
Normal Stress (sigma\\sigma)
0.0 MPa
Deformation (δ)
0.000 mm

Stress-Strain Diagram

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Module 6: Stresses in Beams - Theory & Concepts - Stresses Beams

Flexural (Bending) Stress formula, section modulus, horizontal/longitudinal shear stress, and shear flow.

Flexural Stress Distribution

Beam Cross-Section

200mm
100mm
Compression
Tension

Stress Profile (Depth vs Stress)

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Moment of Inertia (II)
66.67 × 10⁶ mm⁴
Section Modulus (SS)
666.67 × 10³ mm³
Max Flexural Stress (σmax\sigma_{max})
22.50 MPa

Module 7: Deflection of Beams - Theory & Concepts

Concept of elastic curve, Double Integration Method, Area-Moment Method, and Superposition Method.

Beam Deflection (Elastic Curve)

Simply supported beam under a Uniformly Distributed Load (UDL).

Maximum Deflection (δmax\delta_{max})
8.14 mm
Typical Allowable (L/240): 20.8 mm
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Module 9: Combined Stresses - Theory & Concepts

Combined axial and flexural loads and eccentrically loaded members.

Eccentrically Loaded Column Visualizer

Combine uniform axial compression with bending stress caused by an eccentric load.

P = 150 kN
e=50
Cross-section: 300mm × 200mm
Left edge (-150)Centroid (0)Right edge (+150)

Stress Distribution across Width (MPa)

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Axial
Bending
Combined
Stress at Left Face (y = -150)
0.00 MPa
(Compression)
Stress at Right Face (y = +150)
-5.00 MPa
(Compression)

Module 9: Combined Stresses - Theory & Concepts - Middle Third Rule

Combined axial and flexural loads and eccentrically loaded members.

Middle-Third Rule Simulation

0

Status

All Compression

Base Width (bb) = 120 units
Kern Limit (b/6b/6) = pm\\pm20 units

When the load PP is applied within the green highlighted Kern (the middle third of the base), the entire cross-section remains in compression (blue distribution).

If the eccentricity ee exceeds b/6b/6, the bending stress (Mc/IMc/I) becomes greater than the uniform axial stress (P/AP/A) on the opposite face, causing tension to develop (red distribution).

Module 10: Columns - Theory & Concepts

Definition and behavior of columns, Euler's formula, effective length factors, and intermediate columns.

Column Buckling Visualizer (Euler's Formula)

Analyze how length, cross-section, and support conditions affect a column's critical buckling load.

P_cr
Effective Length (KLKL)
4.00 m
Weak Axis IminI_{min}
16.7 ×10⁶
Slenderness (KL/rKL/r)
138.6
Fails by Buckling
2056.2 kN

Column Strength Curve (Stress vs Slenderness)

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