Aeroacoustic wind tunnel

The Aeroacoustic Wind Tunnel (AWT), in operation since 2012, is a unique test rig for investigating aeroacoustic phenomena in pipelines and turbomachinery. The closed pipe system is designed for high mass flows and operating pressures and enables the implementation of various components, such as sensor carriers, silencers or rotating stages, under controlled conditions.

Description

Areas of application

  • Aeroacoustics: Investigation of aeroacoustic generation and transport mechanisms

  • Silencers and liners: Testing and optimization of tubular silencers and liner units

  • Measurement technology: Optimization of acoustic and aerodynamic measurement technology and sensors

  • Numerical validation: Validation of numerical calculation procedures and measurement methods such as RMA and beamforming

Main research areas

  • Sound transport mechanisms: Research into sound transport mechanisms in pipelines and turbomachinery

  • Sound fields: Generation of synthetic sound fields using an integrated sound generator unit

  • Mode analysis: Analysis of mode structures and transport mechanisms at various measurement positions

  • Numerical calculation: Use of the AWT as a validation platform for methods such as computational aeroacoustics (CAA)

Measurement technology used

  • Pressure measurement technology: Steady and unsteady measurement systems

  • Microphones: High-precision pressure field microphones for acoustic analysis

  • Flow analysis: CTA/CCA probes for velocity and turbulence measurements

  • PIV: Endoscopic 3-component Particle Image Velocimetry for flow field measurement

  • Traversing units: Radial and circumferential traversing units for high-resolution acoustic measurements

Specifications

Mass Flow Rate 9,2 kg/s
Pressure Ratio 3,2
Diameter Test Section 0,5 m
Range in Reynolds Number 3,1x105 bis 1,2x106
Homogeneous, swirl-free inflow conditions
Low background noise
Acoustic excitation system with 16 azimuthally distributed speakers