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Mitigation of under...
Mitigation of under-expanded supersonic jet noise through stepped nozzles
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- Wei, X. F. (author)
- Nanyang Technol Univ, Sch Mech & Aerosp Engn, 50 Nanyang Ave, Singapore 639798, Singapore.
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- Mariani, Raffaello (author)
- Nanyang Technol Univ, Sch Mech & Aerosp Engn, 50 Nanyang Ave, Singapore 639798, Singapore
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- Chua, L. P. (author)
- Nanyang Technol Univ, Sch Mech & Aerosp Engn, 50 Nanyang Ave, Singapore 639798, Singapore.
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- Lim, H. D. (author)
- Nanyang Technol Univ, Sch Mech & Aerosp Engn, 50 Nanyang Ave, Singapore 639798, Singapore.
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- Lu, Z. B. (author)
- Natl Univ Singapore, Temasek Labs, Singapore 117411, Singapore.
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- Cui, Y. D. (author)
- Natl Univ Singapore, Temasek Labs, Singapore 117411, Singapore.
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- New, T. H. (author)
- Nanyang Technol Univ, Sch Mech & Aerosp Engn, 50 Nanyang Ave, Singapore 639798, Singapore.
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Nanyang Technol Univ, Sch Mech & Aerosp Engn, 50 Nanyang Ave, Singapore 639798, Singapore Nanyang Technol Univ, Sch Mech & Aerosp Engn, 50 Nanyang Ave, Singapore 639798, Singapore (creator_code:org_t)
- Academic Press, 2019
- 2019
- English.
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In: Journal of Sound and Vibration. - : Academic Press. - 0022-460X .- 1095-8568. ; 459
- Related links:
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https://dr.ntu.edu.s...
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https://urn.kb.se/re...
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https://doi.org/10.1...
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Abstract
Subject headings
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- An experimental investigation into noise reduction of supersonic jets through nozzle trailing-edge modifications was conducted, whereby far-field acoustic measurements were captured for two different stepped nozzles under two distinct under-expanded conditions. When compared to a baseline nozzle, results show that stepped nozzles lead to significant noise reductions at certain polar and azimuthal angles. In particular, a maximum noise reduction of 6 dB is observed for the longest stepped nozzle at a nozzle-pressure-ratio of 4 and 0 degrees azimuthal angle. Spectral analysis shows that the noise reduction is mainly due to reduction in broadband shock associated noise and elimination of jet screech phenomenon. Abrupt changes in nozzle lip lengths of the stepped nozzles appear to disrupt acoustic feedback loop, thus resulting in screech cessation. Qualitative schlieren imaging and quantitative schlieren measurements were subsequently performed to correlate the shock structures and density gradient fields with the resulting noise components. Unlike those produced by the baseline nozzle, shock structures generated by the stepped nozzles are highly irregular and the jet plumes undergo discernible deflections. Lastly, the reduction in broadband shock associated noise is related to the lower shock strengths, as demonstrated by the density gradient profiles.
Subject headings
- TEKNIK OCH TEKNOLOGIER -- Maskinteknik -- Strömningsmekanik och akustik (hsv//swe)
- ENGINEERING AND TECHNOLOGY -- Mechanical Engineering -- Fluid Mechanics and Acoustics (hsv//eng)
Keyword
- Supersonic jet
- Jet noise
- Noise reduction
- Schlieren imaging
- Calibrated schlieren
Publication and Content Type
- ref (subject category)
- art (subject category)
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