Control of flow separation from leading edge of a shallow rectangular cylinder through momentum injection
Finding a method to suppress aeroelastic vibrations of a bridge deck is an important research to construct a superlong suspension bridge with the main span longer than 2000 m. For this end, the boundary-layer control method was proposed and a fundamental experimental research was conducted. This met...
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Veröffentlicht in: | Journal of wind engineering and industrial aerodynamics 1999, Vol.83 (1), p.503-514 |
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container_title | Journal of wind engineering and industrial aerodynamics |
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creator | Kubo, Yoshinobu Yukoku, Eijirou J. Modi, Vinod Yamaguchi, Eiki Kato, Kusuo Kawamura, Shin-ichi |
description | Finding a method to suppress aeroelastic vibrations of a bridge deck is an important research to construct a superlong suspension bridge with the main span longer than 2000
m. For this end, the boundary-layer control method was proposed and a fundamental experimental research was conducted. This method was applied to the suppression of torsional flutter of a shallow rectangular prism which was one of typical fundamental configurations of a bridge deck section. The results obtained from measurements of surface pressure distributions and aeroelastic vibration responses showed that the proposed boundary-layer control method through momentum injection was effective for suppressing the torsional flutter of a shallow rectangular prism. |
doi_str_mv | 10.1016/S0167-6105(99)00097-5 |
format | Article |
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m. For this end, the boundary-layer control method was proposed and a fundamental experimental research was conducted. This method was applied to the suppression of torsional flutter of a shallow rectangular prism which was one of typical fundamental configurations of a bridge deck section. The results obtained from measurements of surface pressure distributions and aeroelastic vibration responses showed that the proposed boundary-layer control method through momentum injection was effective for suppressing the torsional flutter of a shallow rectangular prism.</description><identifier>ISSN: 0167-6105</identifier><identifier>EISSN: 1872-8197</identifier><identifier>DOI: 10.1016/S0167-6105(99)00097-5</identifier><language>eng</language><publisher>Elsevier Ltd</publisher><subject>Active control ; Boundary layer ; Boundary layer flow ; Bridge decks ; Cylinders (shapes) ; Dynamic response ; Flutter ; Flutter (aerodynamics) ; Pressure distribution ; Rotor ; Superlong span bridge ; Vibration control</subject><ispartof>Journal of wind engineering and industrial aerodynamics, 1999, Vol.83 (1), p.503-514</ispartof><rights>1999 Elsevier Science B.V.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c339t-4e43980993863710c276ca5ee6888486e7c4fcd7e14318cda4a53fe80a1bd4fe3</citedby><cites>FETCH-LOGICAL-c339t-4e43980993863710c276ca5ee6888486e7c4fcd7e14318cda4a53fe80a1bd4fe3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://www.sciencedirect.com/science/article/pii/S0167610599000975$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>314,776,780,3537,4010,27900,27901,27902,65306</link.rule.ids></links><search><creatorcontrib>Kubo, Yoshinobu</creatorcontrib><creatorcontrib>Yukoku, Eijirou</creatorcontrib><creatorcontrib>J. Modi, Vinod</creatorcontrib><creatorcontrib>Yamaguchi, Eiki</creatorcontrib><creatorcontrib>Kato, Kusuo</creatorcontrib><creatorcontrib>Kawamura, Shin-ichi</creatorcontrib><title>Control of flow separation from leading edge of a shallow rectangular cylinder through momentum injection</title><title>Journal of wind engineering and industrial aerodynamics</title><description>Finding a method to suppress aeroelastic vibrations of a bridge deck is an important research to construct a superlong suspension bridge with the main span longer than 2000
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source | Elsevier ScienceDirect Journals |
subjects | Active control Boundary layer Boundary layer flow Bridge decks Cylinders (shapes) Dynamic response Flutter Flutter (aerodynamics) Pressure distribution Rotor Superlong span bridge Vibration control |
title | Control of flow separation from leading edge of a shallow rectangular cylinder through momentum injection |
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