{"id":1186,"date":"2020-09-17T13:31:09","date_gmt":"2020-09-17T11:31:09","guid":{"rendered":"https:\/\/www.lfm.polimi.it\/?page_id=1186"},"modified":"2020-11-24T10:19:28","modified_gmt":"2020-11-24T09:19:28","slug":"record","status":"publish","type":"page","link":"https:\/\/www.lfm.polimi.it\/?page_id=1186","title":{"rendered":"Corenoise Reduction in Aeroengines"},"content":{"rendered":"<div id=\"pl-1186\"  class=\"panel-layout\" ><div id=\"pg-1186-0\"  class=\"panel-grid panel-has-style\" ><div class=\"siteorigin-panels-stretch panel-row-style panel-row-style-for-1186-0\" data-stretch-type=\"full-stretched\" ><div id=\"pgc-1186-0-0\"  class=\"panel-grid-cell\" ><div id=\"panel-1186-0-0-0\" class=\"so-panel widget widget_sow-headline panel-first-child panel-last-child\" data-index=\"0\" ><div class=\"panel-widget-style panel-widget-style-for-1186-0-0-0\" ><div\n\t\t\t\n\t\t\tclass=\"so-widget-sow-headline so-widget-sow-headline-default-731f8b164bc5-1186 so-widget-fittext-wrapper\"\n\t\t\t data-fit-text-compressor=\"0\"\n\t\t><div class=\"sow-headline-container \">\n\t\t\t\t\t\t\t<h4 class=\"sow-headline\">\n\t\t\t\t\t\tRECORD - Research on COrenoise ReDuction\t\t\t\t\t\t<\/h4>\n\t\t\t\t\t\t\t\t\t\t\t<div class=\"decoration\">\n\t\t\t\t\t\t<div class=\"decoration-inside\"><\/div>\n\t\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n<\/div><\/div><\/div><\/div><\/div><\/div><div id=\"pg-1186-1\"  class=\"panel-grid panel-has-style\" ><div class=\"siteorigin-panels-stretch panel-row-style panel-row-style-for-1186-1\" data-stretch-type=\"full-stretched\" ><div id=\"pgc-1186-1-0\"  class=\"panel-grid-cell panel-grid-cell-empty\" ><\/div><div id=\"pgc-1186-1-1\"  class=\"panel-grid-cell\" ><div id=\"panel-1186-1-1-0\" class=\"so-panel widget widget_sow-image panel-first-child panel-last-child\" data-index=\"1\" ><div\n\t\t\t\n\t\t\tclass=\"so-widget-sow-image so-widget-sow-image-default-c67d20f9f743-1186\"\n\t\t\t\n\t\t>\n<div class=\"sow-image-container\">\n\t\t<img \n\tsrc=\"https:\/\/www.lfm.polimi.it\/wp-content\/uploads\/2020\/11\/Poli-Milano.jpg\" width=\"525\" height=\"394\" srcset=\"https:\/\/www.lfm.polimi.it\/wp-content\/uploads\/2020\/11\/Poli-Milano.jpg 619w, https:\/\/www.lfm.polimi.it\/wp-content\/uploads\/2020\/11\/Poli-Milano-300x225.jpg 300w\" sizes=\"(max-width: 525px) 100vw, 525px\" title=\"Poli Milano\" alt=\"\" \t\tclass=\"so-widget-image\"\/>\n\t<\/div>\n\n<\/div><\/div><\/div><div id=\"pgc-1186-1-2\"  class=\"panel-grid-cell panel-grid-cell-mobile-last\" ><div id=\"panel-1186-1-2-0\" class=\"so-panel widget widget_sow-editor panel-first-child panel-last-child\" data-index=\"2\" ><div\n\t\t\t\n\t\t\tclass=\"so-widget-sow-editor so-widget-sow-editor-base\"\n\t\t\t\n\t\t>\n<div class=\"siteorigin-widget-tinymce textwidget\">\n\t<h3><strong>LFM CONTRIBUTION (industrial partners: AVIO, TURBOMECA,<br \/>\nSNECMA, RRD, RRUK, ITP, ecc.)<\/strong><\/h3>\n<ol>\n<li style=\"list-style-type: none;\">\n<ol>\n<li style=\"list-style-type: none;\">\n<ol>\n<li style=\"text-align: justify;\">\n<h3>Provide turbine unsteady flow field at different operating point to support unsteady numerical simulations for noise radiation and propagation<\/h3>\n<\/li>\n<li style=\"text-align: justify;\">\n<h3>Experimental simulation of turbine-combustor aeroacoustic interaction: characterization of temperature (entropy) and pressure disturbances at turbine inlet and their effects on the turbine aerodynamics and aeroacoustics<\/h3>\n<\/li>\n<\/ol>\n<\/li>\n<\/ol>\n<\/li>\n<\/ol>\n<\/div>\n<\/div><\/div><\/div><div id=\"pgc-1186-1-3\"  class=\"panel-grid-cell panel-grid-cell-empty\" ><\/div><\/div><\/div><div id=\"pg-1186-2\"  class=\"panel-grid panel-has-style\" ><div class=\"siteorigin-panels-stretch panel-row-style panel-row-style-for-1186-2\" data-stretch-type=\"full-stretched\" ><div id=\"pgc-1186-2-0\"  class=\"panel-grid-cell panel-grid-cell-empty\" ><\/div><div id=\"pgc-1186-2-1\"  class=\"panel-grid-cell panel-grid-cell-mobile-last\" ><div id=\"panel-1186-2-1-0\" class=\"so-panel widget widget_sow-headline panel-first-child panel-last-child\" data-index=\"3\" ><div\n\t\t\t\n\t\t\tclass=\"so-widget-sow-headline so-widget-sow-headline-default-06624dc96049-1186\"\n\t\t\t\n\t\t><div class=\"sow-headline-container \">\n\t\t\t\t\t\t\t<h1 class=\"sow-headline\">\n\t\t\t\t\t\tSelected references\t\t\t\t\t\t<\/h1>\n\t\t\t\t\t\t\t\t\t\t\t<div class=\"decoration\">\n\t\t\t\t\t\t<div class=\"decoration-inside\"><\/div>\n\t\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n<\/div><\/div><\/div><div id=\"pgc-1186-2-2\"  class=\"panel-grid-cell panel-grid-cell-empty\" ><\/div><\/div><\/div><div id=\"pg-1186-3\"  class=\"panel-grid panel-has-style\" ><div class=\"siteorigin-panels-stretch panel-row-style panel-row-style-for-1186-3\" data-stretch-type=\"full-stretched\" ><div id=\"pgc-1186-3-0\"  class=\"panel-grid-cell panel-grid-cell-empty\" ><\/div><div id=\"pgc-1186-3-1\"  class=\"panel-grid-cell panel-grid-cell-mobile-last\" ><div id=\"panel-1186-3-1-0\" class=\"so-panel widget widget_sow-editor panel-first-child panel-last-child\" data-index=\"4\" ><div\n\t\t\t\n\t\t\tclass=\"so-widget-sow-editor so-widget-sow-editor-base\"\n\t\t\t\n\t\t>\n<div class=\"siteorigin-widget-tinymce textwidget\">\n\t<ul>\n<li>\n<h3 style=\"text-align: justify;\"><em>Notaristefano A.,Gaetani P<\/em>., <strong>Design and commissioning of a Combustor Simulator featuring Swirl and Entropy Wave Generator<\/strong>, Int. J. Turbomach. Propuls. Power 2020<\/h3>\n<\/li>\n<li style=\"text-align: justify;\">\n<h3><em>Persico, G; Gaetani, P; Spinelli, A.<\/em> <strong>Assessment of synthetic entropy waves for indirect combustion noise experiments in gas turbines<\/strong>. Exp Therm Fluid Sci 2017, 88, 376-388<\/h3>\n<\/li>\n<li style=\"text-align: justify;\">\n<h3><em>Gaetani, P; Persico, G; Spinelli, A<\/em>. <strong>Coupled effect of expansion ratio and blade loading on the aerodynamics of a high-pressure gas turbine<\/strong>. Appl. Sci 2017, 7, 259<\/h3>\n<\/li>\n<li style=\"text-align: justify;\">\n<h3><em>Persico, G; Gaetani, P; Paradiso, B.<\/em> <strong>Estimation of turbulence by single-sensor pressure probes<\/strong>. XIX Biannual Symposium on Measuring Techniques in Turbomachinery 2008<\/h3>\n<\/li>\n<\/ul>\n<h3 style=\"text-align: justify;\"><\/h3>\n<\/div>\n<\/div><\/div><\/div><div id=\"pgc-1186-3-2\"  class=\"panel-grid-cell panel-grid-cell-empty\" ><\/div><\/div><\/div><\/div>","protected":false},"excerpt":{"rendered":"<p>LFM CONTRIBUTION (industrial partners: AVIO, TURBOMECA, SNECMA, RRD, RRUK, ITP, ecc.) Provide turbine unsteady flow field at different operating point to support unsteady numerical simulations for noise radiation and propagation Experimental simulation of turbine-combustor aeroacoustic interaction: characterization of temperature (entropy) and pressure disturbances at turbine inlet and their effects on the turbine aerodynamics and aeroacoustics<\/p>\n","protected":false},"author":1,"featured_media":0,"parent":0,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"","meta":{"footnotes":""},"class_list":["post-1186","page","type-page","status-publish","hentry"],"_links":{"self":[{"href":"https:\/\/www.lfm.polimi.it\/index.php?rest_route=\/wp\/v2\/pages\/1186","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/www.lfm.polimi.it\/index.php?rest_route=\/wp\/v2\/pages"}],"about":[{"href":"https:\/\/www.lfm.polimi.it\/index.php?rest_route=\/wp\/v2\/types\/page"}],"author":[{"embeddable":true,"href":"https:\/\/www.lfm.polimi.it\/index.php?rest_route=\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/www.lfm.polimi.it\/index.php?rest_route=%2Fwp%2Fv2%2Fcomments&post=1186"}],"version-history":[{"count":0,"href":"https:\/\/www.lfm.polimi.it\/index.php?rest_route=\/wp\/v2\/pages\/1186\/revisions"}],"wp:attachment":[{"href":"https:\/\/www.lfm.polimi.it\/index.php?rest_route=%2Fwp%2Fv2%2Fmedia&parent=1186"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}