Aeroacoustic interaction in high-velocity jet with a thin obstacle
The work is devoted to the investigation of the influence of the thin obstacle presence in the high-speed jet flow on its characteristics. Interest in this phenomenon is caused by the fact that during the transonic jet flow parameters probe measurements it was noted, that a growth of low-frequency p...
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creator | Gubanov, D. A. Zapryagaev, V. I. Kiselev, N. P. Kundasev, S. G. |
description | The work is devoted to the investigation of the influence of the thin obstacle presence in the high-speed jet flow on its characteristics. Interest in this phenomenon is caused by the fact that during the transonic jet flow parameters probe measurements it was noted, that a growth of low-frequency pulsations, tonal and discrete tones appear in the acoustic noise when a pylon is immersed. It is established that discrete and tonal components change their frequency as the distance from a thin obstacle to the nozzle exit is changed. The existence of a mechanism for transferring perturbations from the pylon is shown, which consists in the fact that pulsations from the pylon close the self-oscillating loop through acoustic radiation propagating from the jet through the surrounding medium to jet root. |
doi_str_mv | 10.1063/1.5065296 |
format | Conference Proceeding |
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A. ; Zapryagaev, V. I. ; Kiselev, N. P. ; Kundasev, S. G.</creator><contributor>Fomin, Vasily</contributor><creatorcontrib>Gubanov, D. A. ; Zapryagaev, V. I. ; Kiselev, N. P. ; Kundasev, S. G. ; Fomin, Vasily</creatorcontrib><description>The work is devoted to the investigation of the influence of the thin obstacle presence in the high-speed jet flow on its characteristics. Interest in this phenomenon is caused by the fact that during the transonic jet flow parameters probe measurements it was noted, that a growth of low-frequency pulsations, tonal and discrete tones appear in the acoustic noise when a pylon is immersed. It is established that discrete and tonal components change their frequency as the distance from a thin obstacle to the nozzle exit is changed. The existence of a mechanism for transferring perturbations from the pylon is shown, which consists in the fact that pulsations from the pylon close the self-oscillating loop through acoustic radiation propagating from the jet through the surrounding medium to jet root.</description><identifier>ISSN: 0094-243X</identifier><identifier>EISSN: 1551-7616</identifier><identifier>DOI: 10.1063/1.5065296</identifier><identifier>CODEN: APCPCS</identifier><language>eng</language><publisher>Melville: American Institute of Physics</publisher><subject>Acoustic noise ; Acoustic propagation ; Aeroacoustics ; Jet flow ; Nozzles ; Sound waves</subject><ispartof>AIP Conference Proceedings, 2018, Vol.2027 (1)</ispartof><rights>Author(s)</rights><rights>2018 Author(s). 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G.</creatorcontrib><title>Aeroacoustic interaction in high-velocity jet with a thin obstacle</title><title>AIP Conference Proceedings</title><description>The work is devoted to the investigation of the influence of the thin obstacle presence in the high-speed jet flow on its characteristics. Interest in this phenomenon is caused by the fact that during the transonic jet flow parameters probe measurements it was noted, that a growth of low-frequency pulsations, tonal and discrete tones appear in the acoustic noise when a pylon is immersed. It is established that discrete and tonal components change their frequency as the distance from a thin obstacle to the nozzle exit is changed. The existence of a mechanism for transferring perturbations from the pylon is shown, which consists in the fact that pulsations from the pylon close the self-oscillating loop through acoustic radiation propagating from the jet through the surrounding medium to jet root.</description><subject>Acoustic noise</subject><subject>Acoustic propagation</subject><subject>Aeroacoustics</subject><subject>Jet flow</subject><subject>Nozzles</subject><subject>Sound waves</subject><issn>0094-243X</issn><issn>1551-7616</issn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2018</creationdate><recordtype>conference_proceeding</recordtype><recordid>eNp9kM1LAzEQxYMoWKsH_4MFb8LWTD422WMtfkHBi4K3MJtm3ZTarEla6X_vlha8eZoH8-PNvEfINdAJ0IrfwUTSSrK6OiEjkBJKVUF1SkaU1qJkgn-ck4uUlpSyWik9IvdTFwPasEnZ28Kvs4tosw_rQRed_-zKrVsF6_OuWLpc_PjcFVjkbtiGJmW0K3dJzlpcJXd1nGPy_vjwNnsu569PL7PpvOyZ1rmUQjbc2oYKoI1uUDMr6kbbViuODFupFy3lleAtaqwlggIGTnOttFoAMD4mNwffPobvjUvZLMMmroeThgHTjMpa8IG6PVBpeBr3SUwf_RfGnQFq9h0ZMMeO_oO3If6Bpl-0_BdZ8Was</recordid><startdate>20181102</startdate><enddate>20181102</enddate><creator>Gubanov, D. A.</creator><creator>Zapryagaev, V. I.</creator><creator>Kiselev, N. P.</creator><creator>Kundasev, S. G.</creator><general>American Institute of Physics</general><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20181102</creationdate><title>Aeroacoustic interaction in high-velocity jet with a thin obstacle</title><author>Gubanov, D. A. ; Zapryagaev, V. I. ; Kiselev, N. P. ; Kundasev, S. G.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-p288t-545b3ccb0410b8ba82c49b8cf873a2af58df03643fa8a95a17121e838787d1123</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2018</creationdate><topic>Acoustic noise</topic><topic>Acoustic propagation</topic><topic>Aeroacoustics</topic><topic>Jet flow</topic><topic>Nozzles</topic><topic>Sound waves</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Gubanov, D. A.</creatorcontrib><creatorcontrib>Zapryagaev, V. I.</creatorcontrib><creatorcontrib>Kiselev, N. P.</creatorcontrib><creatorcontrib>Kundasev, S. G.</creatorcontrib><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Gubanov, D. A.</au><au>Zapryagaev, V. I.</au><au>Kiselev, N. P.</au><au>Kundasev, S. G.</au><au>Fomin, Vasily</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Aeroacoustic interaction in high-velocity jet with a thin obstacle</atitle><btitle>AIP Conference Proceedings</btitle><date>2018-11-02</date><risdate>2018</risdate><volume>2027</volume><issue>1</issue><issn>0094-243X</issn><eissn>1551-7616</eissn><coden>APCPCS</coden><abstract>The work is devoted to the investigation of the influence of the thin obstacle presence in the high-speed jet flow on its characteristics. Interest in this phenomenon is caused by the fact that during the transonic jet flow parameters probe measurements it was noted, that a growth of low-frequency pulsations, tonal and discrete tones appear in the acoustic noise when a pylon is immersed. It is established that discrete and tonal components change their frequency as the distance from a thin obstacle to the nozzle exit is changed. The existence of a mechanism for transferring perturbations from the pylon is shown, which consists in the fact that pulsations from the pylon close the self-oscillating loop through acoustic radiation propagating from the jet through the surrounding medium to jet root.</abstract><cop>Melville</cop><pub>American Institute of Physics</pub><doi>10.1063/1.5065296</doi><tpages>5</tpages><oa>free_for_read</oa></addata></record> |
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subjects | Acoustic noise Acoustic propagation Aeroacoustics Jet flow Nozzles Sound waves |
title | Aeroacoustic interaction in high-velocity jet with a thin obstacle |
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