Adjust outer radius, bore, rotational speed and material to visualize radial stress σr and hoop stress σθ profiles in real time. Burst speed and safety factor are computed automatically.
The governing equations for stress in a rotating disk come from elasticity theory, balancing centrifugal body forces. For a solid disk (no central bore), the radial and hoop stresses vary with the radius $r$.
$$ \sigma_r = \frac{3+\nu}{8}\rho\omega^2(R^2 - r^2) $$ $$ \sigma_\theta = \frac{3+\nu}{8}\rho\omega^2 R^2 - \frac{1+3\nu}{8}\rho\omega^2 r^2 $$Where:
$\sigma_r, \sigma_\theta$ = Radial & Hoop Stress [Pa]
$\rho$ = Material Density [kg/m³]
$\omega$ = Angular Velocity [rad/s] ($\omega = 2\pi N / 60$)
$R$ = Outer Radius [m]
$r$ = Radial coordinate [m] (0 at center)
$\nu$ = Poisson's Ratio
Note: At the center ($r=0$), $\sigma_r = \sigma_\theta$.
For an annular disk (with a bore of radius $r_i$), the stresses are expressed using Lamé constants A and B, determined by boundary conditions (radial stress = 0 at both inner and outer free surfaces).
$$ \sigma_r = A - \frac{B}{r^2}- \frac{3+\nu}{8}\rho\omega^2 r^2 $$ $$ \sigma_\theta = A + \frac{B}{r^2}- \frac{1+3\nu}{8}\rho\omega^2 r^2 $$Physical Meaning: The $A \pm B/r^2$ terms represent the static pressure solution, while the terms with $\omega^2$ are the dynamic loading from rotation. The bore creates a stress concentration, making the maximum hoop stress occur at the inner radius, which is often the design-limiting factor.
Centrifuge Rotors in Biotech & Chemistry: High-speed centrifuges separate particles by density. A rotor failure at 50,000+ RPM is catastrophic. Engineers use this exact analysis to select materials like titanium alloys and to determine safe operational speeds well below the burst speed, often incorporating a large safety factor.
Flywheel Energy Storage: Modern flywheels spin in a vacuum on magnetic bearings to store kinetic energy. Maximizing rotational speed is key to energy density, but it's directly limited by the tensile strength of the composite rotor. Stress analysis ensures the rotor operates within its fatigue limits for thousands of cycles.
Turbine & Compressor Disks in Jet Engines: The disks that hold turbine blades spin at extreme speeds under high temperatures. Centrifugal stress analysis is combined with thermal stress models. The bore area is critical and is often reinforced, and precise analysis prevents costly and dangerous "disk burst" failures.
Automotive Brake Disks (Rotors): While primarily designed for thermal loads, brake disks also experience centrifugal stresses during high-speed vehicle operation. Understanding the stress profile helps in designing cooling vanes and ensuring structural integrity, especially in performance racing applications.
When you start using this tool, there are several pitfalls that are easy to fall into, especially for CAE beginners. First is the misconception that "as long as the stress is below the material's yield strength, it's safe." While burst speed is indeed calculated from the yield stress, fatigue failure is a major concern in real-world applications. For instance, a centrifuge rotor spinning at 100,000 rpm can fail due to crack growth from cyclic loading, even if the maximum stress is below 50% of the yield strength. After checking the safety factor with this tool, you must next consider fatigue life.
Next, unit errors in parameter input. This is extremely common. The tool performs calculations internally using SI units (m, kg, rad/s), but design drawings typically use mm for dimensions and rpm for rotational speed. For example, if you inadvertently input an outer diameter of 100mm as "100" (instead of the correct 0.1), the calculated stress will be off by a factor of 10,000, showing a deceptively safe result that could lead to a major failure. Always perform a sanity check after inputting values to ensure the resulting stress is within a reasonable order of magnitude (e.g., tens to hundreds of MPa for steel).
Finally, it's crucial to understand the limitations of the "thin disk" theory. The fundamental equations used by this tool assume a constant and relatively small disk thickness. However, actual turbine disks have significant thickness variations at the hub and blade attachment regions. For such complex geometries, the tool's results are only a first-order approximation. After using the tool to check the stress concentration at the inner bore, the standard practice is to use that value as a reference and perform shape optimization with more detailed 3D FEM analysis.
Steel rotor: radius 150 mm, density 7.85 g/cm³, E=200 GPa, yield=400 MPa. At 10,000 rpm operating speed, radial stress σr_max=45 MPa (outer surface), hoop stress σθ_max=185 MPa (inner bore), burst speed=28,500 rpm, safety factor SF=2.85. Maximum radial displacement u=0.32 mm. Von Mises equivalent stress at bore reaches 210 MPa, margin to yield is 190 MPa (47.5% capacity available).