t/r_i < 0.1 → Thin-wall approximation valid
t/r_i ≥ 0.1 → Thick-wall (Lamé required)
Real-time calculation of through-wall stress distributions in pressure vessels using the Lamé equations. Automatic thin/thick-wall classification, ASME minimum wall thickness evaluation, and von Mises stress distribution visualization.
High-Pressure Gas Vessels and CNG Tanks: Pressure-vessel stress checks are essential for automotive fuel tanks and industrial gas cylinders. Internal pressure and material strength are used to determine a safe minimum wall thickness and confirm that stresses remain within allowable limits.
Chemical Plant Piping and Reactors: Shells used in high-temperature, high-pressure chemical processes require wall-thickness decisions that include corrosion allowance and periodic safety evaluations.
Hydraulic and Pneumatic Cylinders: Hydraulic cylinder tubes in construction equipment and automated factories experience repeated pressure loading, so wall thickness must be selected with fatigue strength in mind.
Energy Systems: Reactor pressure vessels, geothermal piping, and high-temperature steam lines require very high safety margins. This calculation is a useful baseline check for those design studies.
It is easy to think that the thin-wall or thick-wall classification depends only on diameter and thickness. In real design, material yield strength, safety factor, and temperature-related strength reduction also matter. A simple geometry ratio is not enough for high-temperature creep or fatigue design.
The Lamé equations are sometimes associated only with internal pressure, but external pressure and thermal stress can also be included when the boundary conditions are set correctly. For double-wall or combined-pressure structures, incorrect boundary conditions can shift the stress distribution significantly.
Von Mises stress is often assumed to peak at the inner wall. In thick-walled cases, however, shear effects near the outer wall can produce a higher equivalent stress. When pressure and axial load act together, do not overlook possible stress concentration away from the inner surface.
$$\sigma_\theta(r) = \frac{p_i r_i^2}{r_o^2 - r_i^2}\!\left(1 + \frac{r_o^2}{r^2}\right)$$
Maximum at the inner wall (r = r_i).
$$\sigma_r(r) = \frac{p_i r_i^2}{r_o^2 - r_i^2}\!\left(1 - \frac{r_o^2}{r^2}\right)$$
Equal to −p_i at the inner wall, zero at the outer wall (when p_o = 0).
$$t_{\min}= \frac{p \cdot R}{S \cdot E - 0.6p}$$
S = σ_Y / 3 (allowable stress), E = 1 (seamless)
$$\sigma_{vM}= \sqrt{\sigma_\theta^2 - \sigma_\theta\sigma_r + \sigma_r^2}$$
Plane stress approximation (axial stress treated separately if required).
The fundamental governing equation for stress in a thick-walled cylinder under pressure is derived from Lamé's theory. It gives the tangential (hoop) stress at any radial position `r`.
$$ \sigma_\theta(r) = \frac{p_i r_i^2 - p_o r_o^2}{r_o^2 - r_i^2}+ \frac{(p_i - p_o) r_i^2 r_o^2}{(r_o^2 - r_i^2) r^2}$$Where:
$\sigma_\theta(r)$ = Hoop stress at radius `r` [MPa]
$p_i$ = Internal pressure [MPa]
$p_o$ = External pressure (often 0) [MPa]
$r_i$ = Inner radius [mm]
$r_o$ = Outer radius ($r_i + t$) [mm]
$r$ = Radial coordinate where stress is calculated [mm]
For the simpler thin-wall case (where $t/r_i < 0.1$), the stress is assumed constant and is given by the Barlow formula, a simplified version of the Lamé equation.
$$ \sigma_\theta = \frac{p_i r_i}{t} $$This shows the direct proportionality: stress increases with higher pressure or larger radius, and decreases with thicker walls. The physical meaning is that the hoop stress resists the bursting force trying to split the cylinder lengthwise.
Industrial Gas Storage: High-pressure vessels for storing oxygen, nitrogen, or hydrogen must be meticulously designed. Engineers use thick-wall analysis to ensure the inner wall stress does not exceed the fatigue limit of materials like chrome-molybdenum steel, preventing catastrophic failure over thousands of pressure cycles.
Chemical Reactors: Vessels in petrochemical plants often operate at high temperatures and pressures while containing corrosive fluids. Stress analysis determines the minimum wall thickness, and material selection (like SUS316L stainless steel) balances strength with corrosion resistance.
Hydraulic Systems: Accumulators and manifolds in heavy machinery operate under pulsating high pressure. Accurate thick-wall calculation is crucial to prevent fatigue cracks, especially at threaded ports or other stress concentration features not shown in this basic model.
Aerospace Propulsion: Rocket motor casings and fuel lines are extreme examples of pressure vessels. They are designed as thin-wall structures using high-strength, lightweight materials like titanium or composites to minimize weight while containing immense combustion pressures.
Model assumptions: The mathematical model used here relies on simplifying assumptions such as linearity, homogeneity, and isotropy. Always verify that your real system satisfies these assumptions before applying results directly to design decisions.
Units and scale: Many calculation errors arise from unit conversion mistakes or order-of-magnitude errors. Pay close attention to the units shown next to each parameter input.
Validating results: Always sanity-check simulator output against physical intuition or hand calculations. If a result seems unexpected, review your input parameters or verify with an independent method.
Structural & Mechanical Engineering: Solid mechanics, elasticity theory, and materials science form the foundation for many of the governing equations used here.
Fluid & Thermal Engineering: Fluid dynamics and heat transfer share similar mathematical structures (conservation equations, boundary-value problems) and frequently appear in multi-physics problems alongside structural analysis.
Control & Systems Engineering: Dynamic system analysis, state-space methods, and signal processing connect to the time-dependent behaviors modeled in this simulator.