Stress relaxation (const. ε):
$$\sigma(t) = \frac{\sigma_0}{\left[1 + E A n \sigma_0^{n-1}t\right]^{1/n}}$$Compute creep strain and stress relaxation in real time via the Norton power law ε̇=Aσⁿexp(-Q/RT). Select 316SS or IN718 presets, adjust temperature, and visualize Arrhenius-corrected multi-temperature curves.
Stress relaxation (const. ε):
$$\sigma(t) = \frac{\sigma_0}{\left[1 + E A n \sigma_0^{n-1}t\right]^{1/n}}$$The simulator uses the Norton Power Law (Secondary Creep Law) to model the steady-state creep strain rate. This equation captures how the rate depends on applied stress and temperature.
$$\dot{\varepsilon}_{cr}= A\sigma^n \exp\!\left(-\frac{Q}{RT}\right)$$Where:
• $\dot{\varepsilon}_{cr}$: Steady-state creep strain rate (1/s)
• $A$: Material constant (pre-exponential factor)
• $\sigma$: Applied stress (MPa)
• $n$: Stress exponent (unitless, from slider)
• $Q$: Activation energy for creep (J/mol, from slider)
• $R$: Universal gas constant (8.314 J/mol·K)
• $T$: Absolute temperature (Kelvin = °C + 273.15)
The exponential term $\exp(-Q/RT)$ is the Arrhenius factor, governing the dramatic effect of temperature.
For stress relaxation, we assume the total strain (elastic + creep) is constant. As creep strain increases, elastic strain must decrease, which in turn reduces the stress. Solving this condition gives the stress as a function of time.
$$\sigma(t) = \frac{\sigma_0}{\left[1 + E A n \sigma_0^{\,n-1}t \exp\!\left(-\frac{Q}{RT}\right) \right]^{1/n}}$$Where:
• $\sigma(t)$: Relaxing stress at time $t$ (MPa)
• $\sigma_0$: Initial stress (MPa, from slider)
• $E$: Elastic modulus (GPa, from slider)
• $t$: Time (hours)
• Other terms as defined above.
This equation shows how the initial stress $\sigma_0$ decays over time. The rate of decay depends critically on $E$, $n$, and the temperature through the exponential term.
Jet Engine & Gas Turbine Blades: These components operate under extreme centrifugal stress and temperatures over 1000°C. Creep deformation limits their service life. Engineers use models like the Norton law to predict blade elongation and prevent catastrophic failure, scheduling maintenance based on calculated creep life.
Nuclear Reactor Components: Fuel cladding, heat exchangers, and pressure vessels are subjected to high temperature, stress, and radiation for decades. Stress relaxation in bolts and fasteners must be accounted for to maintain structural integrity and leak-tightness over the plant's lifetime.
Power Plant Steam Pipes: Superheated steam pipes carry high-pressure steam at temperatures where creep is significant. Engineers monitor creep strain to schedule pipe replacement before wall thinning leads to rupture, ensuring plant safety and preventing unplanned outages.
Electronic Solder Joints: Even at relatively low "room temperature," the homologous temperature for solder is high. Under constant stress from thermal expansion mismatches, solder joints can creep, leading to eventual electrical failure in circuits. This is a key reliability concern in microelectronics.
When you start using this simulator, there are a few points that are easy to stumble on, especially for CAE beginners. First and foremost, keep in mind that Norton's Law is not a universal solution. This equation primarily describes the region known as "steady-state creep (secondary creep)". Real materials also include initial "primary creep" and "tertiary creep" just before rupture, so consider this tool's results as indicative of steady-state tendencies. For instance, if you need to precisely predict strain after 1000 hours, you often need to separately account for the contribution of primary creep.
Next, handling the material constants (A, n, Q). The preset values are representative, but even for the same "316SS", the numbers can vary based on manufacturing lot or heat treatment history. When using it for actual design work, the golden rule is to use constants you've fitted yourself from measured data of the target material. Also, while the temperature dependence is corrected by the Arrhenius term, it's easy to forget that Young's modulus E also decreases with temperature. In this simulator, E is fixed, but in actual stress relaxation calculations, if you don't use the E value corresponding to the operating temperature, you'll underestimate the relaxation rate, so be careful.