Gößling, Jan and Ahlefeldt, Thomas and Hilfer, Michael (2020) Experimental Validation of Unsteady Pressure-Sensitive Paint for Acoustic Applications. Experimental Thermal and Fluid Science, 112 (109915), pp. 1-13. Elsevier. doi: 10.1016/j.expthermflusci.2019.109915. ISSN 0894-1777.
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Official URL: https://doi.org/10.1016/j.expthermflusci.2019.109915
Abstract
Fast response Pressure-Sensitive Paint (iPSP) developed at the German Aerospace Center (DLR) in Göttingen is evaluated for measurements of acoustic pressure distributions. A test facility is constructed, which allows to measure these acoustic pressure distributions with iPSP. The aim of this evaluation is to detect pressure amplitudes below 100 Pa with sinusoidal and white noise acoustic excitation between 1 and 4 kHz. The following data analysis methods are applied to increase the signal-to-noise ratio (SNR): phase averaging, proper orthogonal decomposition (POD), dynamic mode decomposition (DMD), and fast Fourier transform (FFT). DMD is identified to be very powerful in extracting acoustic pressure fluctuations and eliminating image noise, but FFT achieves comparable results in this application. The used measurement setup combined with the DMD or FFT are capable of detecting pressure levels below 11 Pa or 114 dB sound pressure level (SPL) in cases with white noise excitation with detected mode frequencies up to 4615 Hz. The minimal detectable pressure limit during this investigation is 5 Pa or 108 dB (SPL) at 1318 Hz and sinusoidal acoustic excitation. The results from iPSP are compared to conventional measurement technique, flush with the surface mounted microphones, with good agreement.
| Item URL in elib: | https://elib.dlr.de/137897/ | ||||||||||||||||
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| Document Type: | Article | ||||||||||||||||
| Additional Information: | Paper-DOI: 10.1016/j.expthermflusci.2019.109915 | ||||||||||||||||
| Title: | Experimental Validation of Unsteady Pressure-Sensitive Paint for Acoustic Applications | ||||||||||||||||
| Authors: |
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| Date: | 1 April 2020 | ||||||||||||||||
| Journal or Publication Title: | Experimental Thermal and Fluid Science | ||||||||||||||||
| Refereed publication: | Yes | ||||||||||||||||
| Open Access: | Yes | ||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||
| In SCOPUS: | Yes | ||||||||||||||||
| In ISI Web of Science: | Yes | ||||||||||||||||
| Volume: | 112 | ||||||||||||||||
| DOI: | 10.1016/j.expthermflusci.2019.109915 | ||||||||||||||||
| Page Range: | pp. 1-13 | ||||||||||||||||
| Editors: |
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| Publisher: | Elsevier | ||||||||||||||||
| Series Name: | ScienceDirect | ||||||||||||||||
| ISSN: | 0894-1777 | ||||||||||||||||
| Status: | Published | ||||||||||||||||
| Keywords: | Pressure Sensitive Paint, acoustic, surface measurement, data analysis, Proper Orthogonal Decomposition, Dynamic Mode Decomposition, DMD, POD, FFT, iPSP, SPL | ||||||||||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||||||
| HGF - Program: | Aeronautics | ||||||||||||||||
| HGF - Program Themes: | fixed-wing aircraft | ||||||||||||||||
| DLR - Research area: | Aeronautics | ||||||||||||||||
| DLR - Program: | L AR - Aircraft Research | ||||||||||||||||
| DLR - Research theme (Project): | L - Simulation and Validation (old) | ||||||||||||||||
| Location: | Göttingen | ||||||||||||||||
| Institutes and Institutions: | Institute for Aerodynamics and Flow Technology > Experimental Methods, GO | ||||||||||||||||
| Deposited By: | Micknaus, Ilka | ||||||||||||||||
| Deposited On: | 09 Dec 2020 20:30 | ||||||||||||||||
| Last Modified: | 23 Oct 2023 13:42 |
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