What Is the Curle Aeolian Tone & Cylinder Vortex Shedding Noise Calculator?
An aeolian tone is the musical whistling or humming sound produced when wind blows past telephone wires, suspension bridge cables, or automobile antennas.
Curle (1955) extended Lighthill’s theory to show that solid boundaries in flow introduce acoustic dipole sources scaling with the 6th power of velocity (U⁶), far exceeding quadrupole noise at low Mach numbers.
How Does the Curle Aeolian Tone & Cylinder Vortex Shedding Noise Calculator Work?
Flow separation behind a blunt cylinder forms an alternating von Kármán vortex street.
Each shed vortex induces an equal and opposite fluctuating lift force on the cylinder surface, acting as an acoustic dipole radiating sound perpendicular to the flow.
Curle Aeolian Tone & Cylinder Vortex Shedding Noise Calculator Formula & Variables
The core mathematical equation utilized by this calculator is expressed as:
Computes Strouhal vortex shedding frequency and Curle’s aerodynamic dipole sound power scaling with the 6th power of velocity (U⁶).
How to Use the Curle Aeolian Tone & Cylinder Vortex Shedding Noise Calculator
- Input wind speed and cylinder diameter to determine the pitch of the tone.
- Specify cylinder length and listener distance to calculate Sound Pressure Level (SPL).
- Use helical strakes or fairings if shedding tone creates annoying noise or structural fatigue.
Step-by-Step Example Calculation
15 mm Power Cable in 25 m/s Wind
Input Values:
Understanding Your Result
Shedding frequency fs (Hz) indicates the exact musical pitch of the tone.
Peak SPL (dB) occurs at 90° to the wind direction, where dipole radiation is maximized.
Factors That Affect the Result
- Diameter d: Thinner wires shed vortices at higher frequencies (higher pitch); thick bridge cables produce low-frequency thrumming.
- Velocity U: Frequency scales linearly with wind speed; sound power scales with the 6th power (U⁶).
When Should You Use This Calculator?
- Assessing whistling noise on automotive roof racks and antennas.
- Predicting vortex-induced acoustic noise and vibration in heat exchanger tube bundles.
Assumptions & Limitations
- Valid for uniform crossflow in the subcritical laminar boundary layer regime (300 < Re < 10⁵).
Frequently Asked Questions
Calculation Accuracy & Reference Note
Standard aeroacoustics benchmark model.