$$N_c = \frac{60}{2\pi}\sqrt{\frac{k}{m}}\text{ rpm}$$
Unbalance response amplitude:
$$A = \frac{e \cdot r^2}{\sqrt{(1-r^2)^2 + (2\zeta r)^2}}$$
$r = \omega/\omega_c$ (speed ratio)
Enter rotor mass, shaft stiffness, eccentricity, and damping ratio to compute critical speed Nc. Visualize the unbalance response curve and animated whirl orbit to understand resonance behavior.
$$N_c = \frac{60}{2\pi}\sqrt{\frac{k}{m}}\text{ rpm}$$
Unbalance response amplitude:
$$A = \frac{e \cdot r^2}{\sqrt{(1-r^2)^2 + (2\zeta r)^2}}$$
$r = \omega/\omega_c$ (speed ratio)
The simulator uses the Jeffcott rotor model—a point mass on a flexible, massless shaft. The fundamental critical speed is the rotational speed at which the system's natural frequency is excited.
$$N_c = \frac{60}{2\pi}\sqrt{\frac{k}{m}}\ \text{rpm}$$$N_c$ : Critical speed (revolutions per minute). $k$ : Shaft stiffness (N/m). $m$: Rotor mass (kg). This shows the critical speed increases with stiffness and decreases with mass.
When running at any speed, the vibration amplitude due to mass unbalance is calculated. The response depends on the speed ratio, eccentricity, and damping.
$$A = \frac{e \cdot r^2}{\sqrt{(1-r^2)^2 + (2\zeta r)^2}}\quad \text{where}\quad r = \frac{n}{N_c}$$$A$ : Vibration amplitude (m). $e$ : Mass eccentricity (m). $r$ : Speed ratio. $\zeta$ : Damping ratio. The denominator causes the amplitude to peak near $r=1$ (critical speed), but damping ($\zeta$) controls the peak's height.
Turbomachinery Design (Gas Turbines, Compressors): Engineers must calculate critical speeds to ensure the machine's operating range is safely away from them. For instance, a jet engine's high-pressure spool might operate at 15,000 rpm, so designers adjust bearing stiffness and rotor dimensions to push its first critical speed well above or below this range to avoid catastrophic vibration during flight.
API Standard Compliance for Pumps & Fans: Industry standards like API 610 for pumps mandate that critical speeds be at least 20% away from the operating speed. This simulator helps designers quickly check if a proposed rotor design (with its specific mass and stiffness) meets this margin of safety before detailed and expensive prototyping.
Super-Critical Rotor Operation (Large Steam Turbines): Some large rotors must operate above their first critical speed. The key is to accelerate through the critical speed quickly during startup to minimize vibration exposure. The damping and unbalance response calculated here are crucial for planning these transient maneuvers.
Diagnosing Vibration Problems in Maintenance: If a motor or fan develops high vibration at a specific speed, maintenance teams can use this principle to diagnose the issue. By comparing the problem speed to the calculated critical speed, they can determine if they are dealing with a resonance problem (requiring a balance or stiffness change) or another fault like misalignment.
First, the misconception that "the critical speed is a dangerous speed that must never be passed." While it is indeed dangerous to operate steadily at that speed, many high-speed rotating machines are designed with "supercritical operation" in mind. The key is to properly design the damping and to pass through quickly during startup and shutdown. For example, a certain turbo-molecular pump has its first critical speed around 10,000 rpm, but its operating speed is 80,000 rpm. During shutdown, vibration increases momentarily in this 10,000 rpm range, but it can be passed safely thanks to damping design.
Next, setting the "equivalent mass" or "equivalent stiffness" used in simulators. This is often the most challenging part in practice. For instance, when considering a mass (m) concentrated at the center of a shaft, you don't simply substitute the actual rotor mass. You need to add a portion of the shaft's own mass (typically 1/3 to 1/2). For stiffness (k), it's often not just the shaft stiffness but the stiffness of the bearings and support structure that dominates. Be mindful as the type of bearing (ball bearing vs. journal bearing) and oil film stiffness can have a significant impact.
Finally, the idealistic notion that "vibration will disappear if the eccentricity (e) is reduced to zero." In reality, unbalance inevitably occurs due to machining/assembly errors, material inhomogeneity, thermal deformation, and wear during operation. Using the tool to see how amplitude changes with e is for predicting the effect of balance correction. For example, you can qualitatively understand that reducing eccentricity from 10μm to 5μm (balance correction) can nearly halve the amplitude at resonance. Rather than aiming for perfect zero, a cost-effective sense of keeping it within the allowable amplitude limit is crucial.
A 120 kg centrifugal pump rotor on elastomer-damped bearings: mass=120 kg, stiffness=2.5×10⁵ N/m, eccentricity=0.8 mm. Critical speed Nc = (1/2π)√(2.5×10⁵/120) ≈ 730 rpm. At operating speed 1200 rpm (speed ratio 1.64), peak amplitude ≈ 1.2 mm. Operating above 1.5× Nc (1095 rpm) ensures amplitude drops to ~0.5 mm, acceptable for ISO 20816-3 Group 2 machines.