Windkanal
The invention relates to a wind tunnel (1), in particular for aero-acoustic measuring, with closed air conduction and a free jet measuring section, whereby measures are taken to avoid or at least reduce disruptive aerodynamic oscillation. This is achieved, in accordance with the invention, by fittin...
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creator | HEESEN, WILHELM VON, 44575 CASTROP-RAUXEL, DE WICKERN, GERHARD., 85080 GAIMERSHEIM, DE WALLMANN, STEFFEN, 09119 NITZ, DE |
description | The invention relates to a wind tunnel (1), in particular for aero-acoustic measuring, with closed air conduction and a free jet measuring section, whereby measures are taken to avoid or at least reduce disruptive aerodynamic oscillation. This is achieved, in accordance with the invention, by fitting a device, in particular one or several loud speaker units (33-35), to initiate aerodynamic oscillations in opposition of phase. This system makes it possible to avoid in particular the phenomenon that occurs in wind tunnels with closed air conduction and free jet working section (so-called Göttinger type), in the form of low frequency aerodynamic oscillation which develops at certain aerodynamic speeds and is likely to generate resonance inside the tunnel. |
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This is achieved, in accordance with the invention, by fitting a device, in particular one or several loud speaker units (33-35), to initiate aerodynamic oscillations in opposition of phase. This system makes it possible to avoid in particular the phenomenon that occurs in wind tunnels with closed air conduction and free jet working section (so-called Göttinger type), in the form of low frequency aerodynamic oscillation which develops at certain aerodynamic speeds and is likely to generate resonance inside the tunnel.</description><edition>6</edition><language>ger</language><subject>MEASURING ; PHYSICS ; TESTING ; TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES ; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR</subject><creationdate>1998</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19980730&DB=EPODOC&CC=DE&NR=19702390A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19980730&DB=EPODOC&CC=DE&NR=19702390A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HEESEN, WILHELM VON, 44575 CASTROP-RAUXEL, DE</creatorcontrib><creatorcontrib>WICKERN, GERHARD., 85080 GAIMERSHEIM, DE</creatorcontrib><creatorcontrib>WALLMANN, STEFFEN, 09119 NITZ, DE</creatorcontrib><title>Windkanal</title><description>The invention relates to a wind tunnel (1), in particular for aero-acoustic measuring, with closed air conduction and a free jet measuring section, whereby measures are taken to avoid or at least reduce disruptive aerodynamic oscillation. This is achieved, in accordance with the invention, by fitting a device, in particular one or several loud speaker units (33-35), to initiate aerodynamic oscillations in opposition of phase. This system makes it possible to avoid in particular the phenomenon that occurs in wind tunnels with closed air conduction and free jet working section (so-called Göttinger type), in the form of low frequency aerodynamic oscillation which develops at certain aerodynamic speeds and is likely to generate resonance inside the tunnel.</description><subject>MEASURING</subject><subject>PHYSICS</subject><subject>TESTING</subject><subject>TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES</subject><subject>TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1998</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZOAMz8xLyU7MS8zhYWBNS8wpTuWF0twMim6uIc4euqkF-fGpxQWJyal5qSXxLq6GluYGRsaWBo6GxsSoAQCXYRx5</recordid><startdate>19980730</startdate><enddate>19980730</enddate><creator>HEESEN, WILHELM VON, 44575 CASTROP-RAUXEL, DE</creator><creator>WICKERN, GERHARD., 85080 GAIMERSHEIM, DE</creator><creator>WALLMANN, STEFFEN, 09119 NITZ, DE</creator><scope>EVB</scope></search><sort><creationdate>19980730</creationdate><title>Windkanal</title><author>HEESEN, WILHELM VON, 44575 CASTROP-RAUXEL, DE ; WICKERN, GERHARD., 85080 GAIMERSHEIM, DE ; WALLMANN, STEFFEN, 09119 NITZ, DE</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_DE19702390A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>ger</language><creationdate>1998</creationdate><topic>MEASURING</topic><topic>PHYSICS</topic><topic>TESTING</topic><topic>TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES</topic><topic>TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR</topic><toplevel>online_resources</toplevel><creatorcontrib>HEESEN, WILHELM VON, 44575 CASTROP-RAUXEL, DE</creatorcontrib><creatorcontrib>WICKERN, GERHARD., 85080 GAIMERSHEIM, DE</creatorcontrib><creatorcontrib>WALLMANN, STEFFEN, 09119 NITZ, DE</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HEESEN, WILHELM VON, 44575 CASTROP-RAUXEL, DE</au><au>WICKERN, GERHARD., 85080 GAIMERSHEIM, DE</au><au>WALLMANN, STEFFEN, 09119 NITZ, DE</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Windkanal</title><date>1998-07-30</date><risdate>1998</risdate><abstract>The invention relates to a wind tunnel (1), in particular for aero-acoustic measuring, with closed air conduction and a free jet measuring section, whereby measures are taken to avoid or at least reduce disruptive aerodynamic oscillation. This is achieved, in accordance with the invention, by fitting a device, in particular one or several loud speaker units (33-35), to initiate aerodynamic oscillations in opposition of phase. This system makes it possible to avoid in particular the phenomenon that occurs in wind tunnels with closed air conduction and free jet working section (so-called Göttinger type), in the form of low frequency aerodynamic oscillation which develops at certain aerodynamic speeds and is likely to generate resonance inside the tunnel.</abstract><edition>6</edition><oa>free_for_read</oa></addata></record> |
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subjects | MEASURING PHYSICS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR |
title | Windkanal |
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