Estimate blade tip speed, angular motion, and rotor loading fast. Review performance limits using clear engineering outputs for rotating systems.
| Scenario | Diameter (m) | RPM | Tip Speed (m/s) | Tip Speed (km/h) | Mach |
|---|---|---|---|---|---|
| Small Fan Rotor | 0.40 | 1800 | 37.70 | 135.72 | 0.11 |
| Workshop Grinder Wheel | 0.25 | 3450 | 45.16 | 162.59 | 0.13 |
| Industrial Blower | 1.20 | 2400 | 150.80 | 542.89 | 0.44 |
| Turbine Rotor | 2.00 | 3600 | 376.99 | 1357.17 | 1.10 |
1) Angular velocity: ω = 2π × RPM / 60
2) Blade tip speed: V = ω × r
3) Alternate tip speed form: V = π × D × RPM / 60
4) Centripetal acceleration: a = V² / r
5) Mach number: M = V / asound
Where ω is angular velocity, r is radius, D is diameter, V is tip speed, and asound is the local speed of sound.
Blade tip speed is the linear velocity at the outermost edge of a rotating blade. It is important for fans, turbines, propellers, compressors, and safety checks involving dynamic loading and noise.
A larger diameter increases radius, and tip speed rises directly with radius when RPM stays constant. Even moderate diameter growth can produce a large increase in edge velocity.
Yes. This calculator lets you choose either diameter input or radius input. It converts the missing geometric value automatically and uses the same engineering equations.
Mach number helps indicate compressibility effects, noise concerns, and aerodynamic losses. Rotors approaching high Mach values may need more detailed design review and operating limits.
The correction factor multiplies the raw tip speed result. It is useful for adjusted studies, what-if scenarios, model matching, or including a design factor in preliminary analysis.
Yes. Centripetal acceleration relates directly to loading at the blade tip. High values can influence stress, material selection, fatigue performance, and bearing or hub design considerations.
Use m/s for engineering analysis, km/h or mph for easier interpretation, and ft/s where imperial workflows are common. The physical calculation remains the same.
No. It is a strong preliminary calculator for speed and loading checks. Detailed rotor design still needs aerodynamic, thermal, material, vibration, and safety evaluations.
Important Note: All the Calculators listed in this site are for educational purpose only and we do not guarentee the accuracy of results. Please do consult with other sources as well.