Aerodynamic Noise in Control Valves
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When gas or steam flows through a control valve, it generates noise, commonly referred to as "aerodynamic noise." Depending on the valve's size, flow rate, and the differential pressure across it, this noise can become loud enough to be irritating or even harmful to nearby workers. Understanding what causes aerodynamic noise and how to mitigate it is crucial for maintaining a safe and comfortable working environment.
Figure 1. Velocity and Pressure Profile Inside a Control Valve
As the gas passes through the vena contracta, it expands rapidly due to the drop in pressure. Beyond this point, as the pressure rises again, the gas re-compresses. This rapid expansion and subsequent compression create severe turbulence, which is the primary source of aerodynamic noise. The intensity of the noise is closely related to the peak velocity of the gas. At subsonic velocities, the sound intensity in a free jet is proportional to the eighth power of the jet velocity. At supersonic velocities, the generation of shock waves makes the relationship between velocity and sound intensity even more pronounced.
Figure 2. Generation of Aerodynamic Noise in a Control Valve
Figure 1. Velocity and Pressure Profile Inside a Control Valve
Causes of Aerodynamic Noise
The generation of aerodynamic noise begins when gas flows past a restriction in a control valve, causing the velocity to increase and reach a peak at the vena contracta—the point of minimum cross-sectional area in the flow path. According to the law of conservation of energy, when the gas velocity increases, the pressure decreases, leading to the rapid expansion of the gas.As the gas passes through the vena contracta, it expands rapidly due to the drop in pressure. Beyond this point, as the pressure rises again, the gas re-compresses. This rapid expansion and subsequent compression create severe turbulence, which is the primary source of aerodynamic noise. The intensity of the noise is closely related to the peak velocity of the gas. At subsonic velocities, the sound intensity in a free jet is proportional to the eighth power of the jet velocity. At supersonic velocities, the generation of shock waves makes the relationship between velocity and sound intensity even more pronounced.
Figure 2. Generation of Aerodynamic Noise in a Control Valve