Short-time proper orthogonal decomposition of time-resolved schlieren images for transient jet screech characterization
Short-time Proper Orthogonal Decomposition (POD) is proposed as an image-based technique to study the transient jet screech characteristics of moderately under-expanded supersonic jets emanating from a circular baseline and two bevelled nozzles. Time-resolved schlieren imaging of turbulent flow stru...
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sg-ntu-dr.10356-1609042022-08-05T07:32:07Z Short-time proper orthogonal decomposition of time-resolved schlieren images for transient jet screech characterization Lim, Desmond Haoxiang Wei, Xiaofeng Zang, Bin Vevek, U. S. Mariani, Raffaello New, Tze How Cui, Y. D. School of Mechanical and Aerospace Engineering Engineering::Mechanical engineering Flow Diagnostics Schlieren Short-time Proper Orthogonal Decomposition (POD) is proposed as an image-based technique to study the transient jet screech characteristics of moderately under-expanded supersonic jets emanating from a circular baseline and two bevelled nozzles. Time-resolved schlieren imaging of turbulent flow structures were performed with an ultrahigh-speed schlieren setup. Short-time POD was performed by systematically sampling image-series with a short time delay, performing PODs and applying spectral analyses on the first POD mode coefficients, and plotting the peak frequencies from the resulting PSDs into a peak frequency-occurrence count histogram. The results are in good agreement with the near-field noise spectra and wavelet transform analysis of the microphone measurements, which revealed intermittent jet screech occurrences at St=0.25 for both baseline and 30° bevelled jets, while none was detected for the 60° bevelled jet. In particular, the occurrence counts of the frequency bins is proposed as a suitable parameter to characterize the intermittent nature of jet screech, with the frequency bin revealing the jet screech frequency if present. The present study demonstrates the advantage of short-time POD analysis on time-resolved schlieren images over traditional image-based POD methods, which includes computational gains from parallelization, the ability to handle much larger datasets and revealing insights into a transient flow and noise phenomenon. Ministry of Education (MOE) Nanyang Technological University The authors gratefully acknowledge support for the study through a Singapore Ministry of Education AcRF Tier-2 grant (Grant number: MOE2014-T2-1-002), as well as support for the first author through a NTU Nanyang President Graduate Scholarship. 2022-08-05T07:32:06Z 2022-08-05T07:32:06Z 2020 Journal Article Lim, D. H., Wei, X., Zang, B., Vevek, U. S., Mariani, R., New, T. H. & Cui, Y. D. (2020). Short-time proper orthogonal decomposition of time-resolved schlieren images for transient jet screech characterization. Aerospace Science and Technology, 107, 106276-. https://dx.doi.org/10.1016/j.ast.2020.106276 1270-9638 https://hdl.handle.net/10356/160904 10.1016/j.ast.2020.106276 2-s2.0-85093927308 107 106276 en MOE2014-T2-1-002 Aerospace Science and Technology © 2020 Elsevier Masson SAS. All rights reserved. |
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Engineering::Mechanical engineering Flow Diagnostics Schlieren Lim, Desmond Haoxiang Wei, Xiaofeng Zang, Bin Vevek, U. S. Mariani, Raffaello New, Tze How Cui, Y. D. Short-time proper orthogonal decomposition of time-resolved schlieren images for transient jet screech characterization |
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Short-time Proper Orthogonal Decomposition (POD) is proposed as an image-based technique to study the transient jet screech characteristics of moderately under-expanded supersonic jets emanating from a circular baseline and two bevelled nozzles. Time-resolved schlieren imaging of turbulent flow structures were performed with an ultrahigh-speed schlieren setup. Short-time POD was performed by systematically sampling image-series with a short time delay, performing PODs and applying spectral analyses on the first POD mode coefficients, and plotting the peak frequencies from the resulting PSDs into a peak frequency-occurrence count histogram. The results are in good agreement with the near-field noise spectra and wavelet transform analysis of the microphone measurements, which revealed intermittent jet screech occurrences at St=0.25 for both baseline and 30° bevelled jets, while none was detected for the 60° bevelled jet. In particular, the occurrence counts of the frequency bins is proposed as a suitable parameter to characterize the intermittent nature of jet screech, with the frequency bin revealing the jet screech frequency if present. The present study demonstrates the advantage of short-time POD analysis on time-resolved schlieren images over traditional image-based POD methods, which includes computational gains from parallelization, the ability to handle much larger datasets and revealing insights into a transient flow and noise phenomenon. |
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School of Mechanical and Aerospace Engineering |
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School of Mechanical and Aerospace Engineering Lim, Desmond Haoxiang Wei, Xiaofeng Zang, Bin Vevek, U. S. Mariani, Raffaello New, Tze How Cui, Y. D. |
format |
Article |
author |
Lim, Desmond Haoxiang Wei, Xiaofeng Zang, Bin Vevek, U. S. Mariani, Raffaello New, Tze How Cui, Y. D. |
author_sort |
Lim, Desmond Haoxiang |
title |
Short-time proper orthogonal decomposition of time-resolved schlieren images for transient jet screech characterization |
title_short |
Short-time proper orthogonal decomposition of time-resolved schlieren images for transient jet screech characterization |
title_full |
Short-time proper orthogonal decomposition of time-resolved schlieren images for transient jet screech characterization |
title_fullStr |
Short-time proper orthogonal decomposition of time-resolved schlieren images for transient jet screech characterization |
title_full_unstemmed |
Short-time proper orthogonal decomposition of time-resolved schlieren images for transient jet screech characterization |
title_sort |
short-time proper orthogonal decomposition of time-resolved schlieren images for transient jet screech characterization |
publishDate |
2022 |
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https://hdl.handle.net/10356/160904 |
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1743119519580160000 |