Abstract
Measuring the statistics of the wall-pressure fluctuations (WPFs) is essential for understanding and evaluating laminar/turbulent boundary layers and flow-induced noise. The remote microphone probe (RMP) technique is one of the most successful experimental approaches to measuring WPFs. Despite its extensive use in academic and industrial research, the scientific literature currently lacks an evaluation of the RMP influence on the determination of turbulence quantities, such as the WPF spectrum, the convection velocity, and the turbulence coherence length. To fulfill this necessity, this paper analyses the effects of the RMP on the determination of turbulence quantities, including comparisons between the results obtained using RMPs and flush-mounted microphones (FMMs). The RMPs and the FMMs measure the WPFs under a turbulent boundary layer developed on a zero-pressure-gradient flat wall. This study shows that the turbulence quantities determined from RMP measurements are influenced by the RMP setup, i.e., tube length and inner diameter. The tube length affects the phase between RMPs, which impacts the turbulent structure convection velocity estimation, which can be determined correctly by considering the calibrated phase. Furthermore, the tube inner diameter influences the coherence between a pair of RMPs, affecting the calculation of the turbulence correlation length. This research also shows that the turbulence quantities determined from the RMP and the FMM measurements differ, mainly in the coherence between pairs of microphones.
| Original language | English |
|---|---|
| Article number | 109387 |
| Journal | Applied acoustics |
| Volume | 208 |
| DOIs | |
| Publication status | Published - 15 Jun 2023 |
Keywords
- Flow-induced noise
- Flush-mounted microphone
- Remote microphone probe
- Turbulent boundary layer
- Wall-pressure fluctuation measurements
- UT-Hybrid-D
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Dive into the research topics of 'Analysis of the remote microphone probe technique for the determination of turbulence quantities'. Together they form a unique fingerprint.Research output
- 7 Citations
- 2 PhD Thesis - Research UT, graduation UT
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Boundary layer development and flow-induced noise of airfoils: The effect of high inflow turbulence on trailing-edge noise generation
Botero Bolivar, L., 1 Mar 2024, Enschede: University of Twente. 513 p.Research output: Thesis › PhD Thesis - Research UT, graduation UT
Open AccessFile362 Downloads (Pure) -
Broadband Flow-Induced Noise for Airfoils: Inflow Turbulence Distortion Effect on Leading-Edge Noise Generation and Prediction
Dos Santos, F. L., 22 Sept 2023, Enschede, Netherlands: University of Twente. 453 p.Research output: Thesis › PhD Thesis - Research UT, graduation UT
Open AccessFile391 Downloads (Pure)
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