Experimental investigation of the suppression of vortex-induced vibration in four cylinders arranged in a square under different spacing ratios

Abstract A vortex-induced vibration (VIV) is a typical flow-structure interference phenomenon that causes an unsteady flow pattern owing to vortex shedding at or near the structure’s natural frequency, leading to resonant vibrations. VIVs can cause the failure of marine risers owing to premature fat...
Ausführliche Beschreibung

Gespeichert in:

Autor*in:	Lou, Min [verfasserIn] Qian, Gang [verfasserIn] Li, Run [verfasserIn]

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2019

Schlagwörter:	Vortex-induced vibration Suppression Splitter plates Square arrangement Spacing ratio

Übergeordnetes Werk:	Enthalten in: Journal of marine science and technology - Tokyo : Springer, 1995, 25(2019), 2 vom: 30. Mai, Seite 467-481
Übergeordnetes Werk:	volume:25 ; year:2019 ; number:2 ; day:30 ; month:05 ; pages:467-481

Links:	Volltext

DOI / URN:	10.1007/s00773-019-00654-z

Katalog-ID:	SPR039766381

Internformat


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245	1	0	\|a Experimental investigation of the suppression of vortex-induced vibration in four cylinders arranged in a square under different spacing ratios
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520			\|a Abstract A vortex-induced vibration (VIV) is a typical flow-structure interference phenomenon that causes an unsteady flow pattern owing to vortex shedding at or near the structure’s natural frequency, leading to resonant vibrations. VIVs can cause the failure of marine risers owing to premature fatigue, because of which a growing amount of research has attended to them. To investigate the effects of suppressing the VIV of splitter plates on a square array of cylinders under different spacing ratios, cylinders undergoing VIV in a flow with a Reynolds number ranging from 3300 to 6750 were experimentally studied in this paper. The results show that the splitter plate can suppress cross-flow (CF) vibrations as well as in-line flow (IF) vibrations in the cylinders. For cross-flow vibration, the suppression effects of the splitter plate on the upstream cylinders were at their maximum at %$S/D = 5%$ while the effects on downstream cylinders reached this at %$S/D = 6%$, where %$S/D%$ refers to the ratio of the distance between the centers of cylinders to its diameter. For in-line flow vibrations, the effects on upstream and downstream cylinders all reached the maximum at %$S/D = 4%$. The vibrational frequency of the cylinder with splitter plate was also lower than that of the bare cylinder in the flow.
650		4	\|a Vortex-induced vibration \|7 (dpeaa)DE-He213
650		4	\|a Suppression \|7 (dpeaa)DE-He213
650		4	\|a Splitter plates \|7 (dpeaa)DE-He213
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650		4	\|a Spacing ratio \|7 (dpeaa)DE-He213
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700	1		\|a Li, Run \|e verfasserin \|4 aut
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912			\|a GBV_ILN_73
912			\|a GBV_ILN_74
912			\|a GBV_ILN_90
912			\|a GBV_ILN_95
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912			\|a GBV_ILN_105
912			\|a GBV_ILN_110
912			\|a GBV_ILN_120
912			\|a GBV_ILN_138
912			\|a GBV_ILN_150
912			\|a GBV_ILN_151
912			\|a GBV_ILN_152
912			\|a GBV_ILN_161
912			\|a GBV_ILN_170
912			\|a GBV_ILN_171
912			\|a GBV_ILN_187
912			\|a GBV_ILN_213
912			\|a GBV_ILN_224
912			\|a GBV_ILN_230
912			\|a GBV_ILN_250
912			\|a GBV_ILN_267
912			\|a GBV_ILN_281
912			\|a GBV_ILN_285
912			\|a GBV_ILN_293
912			\|a GBV_ILN_370
912			\|a GBV_ILN_602
912			\|a GBV_ILN_636
912			\|a GBV_ILN_702
912			\|a GBV_ILN_2001
912			\|a GBV_ILN_2003
912			\|a GBV_ILN_2004
912			\|a GBV_ILN_2005
912			\|a GBV_ILN_2006
912			\|a GBV_ILN_2007
912			\|a GBV_ILN_2009
912			\|a GBV_ILN_2010
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912			\|a GBV_ILN_2014
912			\|a GBV_ILN_2015
912			\|a GBV_ILN_2020
912			\|a GBV_ILN_2021
912			\|a GBV_ILN_2025
912			\|a GBV_ILN_2026
912			\|a GBV_ILN_2027
912			\|a GBV_ILN_2031
912			\|a GBV_ILN_2034
912			\|a GBV_ILN_2037
912			\|a GBV_ILN_2038
912			\|a GBV_ILN_2039
912			\|a GBV_ILN_2044
912			\|a GBV_ILN_2048
912			\|a GBV_ILN_2049
912			\|a GBV_ILN_2050
912			\|a GBV_ILN_2055
912			\|a GBV_ILN_2057
912			\|a GBV_ILN_2059
912			\|a GBV_ILN_2061
912			\|a GBV_ILN_2064
912			\|a GBV_ILN_2065
912			\|a GBV_ILN_2068
912			\|a GBV_ILN_2070
912			\|a GBV_ILN_2086
912			\|a GBV_ILN_2088
912			\|a GBV_ILN_2093
912			\|a GBV_ILN_2106
912			\|a GBV_ILN_2107
912			\|a GBV_ILN_2108
912			\|a GBV_ILN_2110
912			\|a GBV_ILN_2111
912			\|a GBV_ILN_2112
912			\|a GBV_ILN_2113
912			\|a GBV_ILN_2116
912			\|a GBV_ILN_2118
912			\|a GBV_ILN_2119
912			\|a GBV_ILN_2122
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author_variant	m l ml g q gq r l rl
matchkey_str	article:14378213:2019----::xeietlnetgtooteupesoovreidcdirtoifuclnesragdns
hierarchy_sort_str	2019
bklnumber	38.90 50.92 38.48
publishDate	2019
allfields	10.1007/s00773-019-00654-z doi (DE-627)SPR039766381 (SPR)s00773-019-00654-z-e DE-627 ger DE-627 rakwb eng 550 620 ASE 380 ASE 38.90 bkl 50.92 bkl 38.48 bkl Lou, Min verfasserin aut Experimental investigation of the suppression of vortex-induced vibration in four cylinders arranged in a square under different spacing ratios 2019 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract A vortex-induced vibration (VIV) is a typical flow-structure interference phenomenon that causes an unsteady flow pattern owing to vortex shedding at or near the structure’s natural frequency, leading to resonant vibrations. VIVs can cause the failure of marine risers owing to premature fatigue, because of which a growing amount of research has attended to them. To investigate the effects of suppressing the VIV of splitter plates on a square array of cylinders under different spacing ratios, cylinders undergoing VIV in a flow with a Reynolds number ranging from 3300 to 6750 were experimentally studied in this paper. The results show that the splitter plate can suppress cross-flow (CF) vibrations as well as in-line flow (IF) vibrations in the cylinders. For cross-flow vibration, the suppression effects of the splitter plate on the upstream cylinders were at their maximum at %$S/D = 5%$ while the effects on downstream cylinders reached this at %$S/D = 6%$, where %$S/D%$ refers to the ratio of the distance between the centers of cylinders to its diameter. For in-line flow vibrations, the effects on upstream and downstream cylinders all reached the maximum at %$S/D = 4%$. The vibrational frequency of the cylinder with splitter plate was also lower than that of the bare cylinder in the flow. Vortex-induced vibration (dpeaa)DE-He213 Suppression (dpeaa)DE-He213 Splitter plates (dpeaa)DE-He213 Square arrangement (dpeaa)DE-He213 Spacing ratio (dpeaa)DE-He213 Qian, Gang verfasserin aut Li, Run verfasserin aut Enthalten in Journal of marine science and technology Tokyo : Springer, 1995 25(2019), 2 vom: 30. Mai, Seite 467-481 (DE-627)300185499 (DE-600)1481609-X 1437-8213 nnns volume:25 year:2019 number:2 day:30 month:05 pages:467-481 https://dx.doi.org/10.1007/s00773-019-00654-z lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER SSG-OPC-GGO SSG-OPC-ASE GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_267 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2070 GBV_ILN_2086 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2116 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 38.90 ASE 50.92 ASE 38.48 ASE AR 25 2019 2 30 05 467-481
spelling	10.1007/s00773-019-00654-z doi (DE-627)SPR039766381 (SPR)s00773-019-00654-z-e DE-627 ger DE-627 rakwb eng 550 620 ASE 380 ASE 38.90 bkl 50.92 bkl 38.48 bkl Lou, Min verfasserin aut Experimental investigation of the suppression of vortex-induced vibration in four cylinders arranged in a square under different spacing ratios 2019 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract A vortex-induced vibration (VIV) is a typical flow-structure interference phenomenon that causes an unsteady flow pattern owing to vortex shedding at or near the structure’s natural frequency, leading to resonant vibrations. VIVs can cause the failure of marine risers owing to premature fatigue, because of which a growing amount of research has attended to them. To investigate the effects of suppressing the VIV of splitter plates on a square array of cylinders under different spacing ratios, cylinders undergoing VIV in a flow with a Reynolds number ranging from 3300 to 6750 were experimentally studied in this paper. The results show that the splitter plate can suppress cross-flow (CF) vibrations as well as in-line flow (IF) vibrations in the cylinders. For cross-flow vibration, the suppression effects of the splitter plate on the upstream cylinders were at their maximum at %$S/D = 5%$ while the effects on downstream cylinders reached this at %$S/D = 6%$, where %$S/D%$ refers to the ratio of the distance between the centers of cylinders to its diameter. For in-line flow vibrations, the effects on upstream and downstream cylinders all reached the maximum at %$S/D = 4%$. The vibrational frequency of the cylinder with splitter plate was also lower than that of the bare cylinder in the flow. Vortex-induced vibration (dpeaa)DE-He213 Suppression (dpeaa)DE-He213 Splitter plates (dpeaa)DE-He213 Square arrangement (dpeaa)DE-He213 Spacing ratio (dpeaa)DE-He213 Qian, Gang verfasserin aut Li, Run verfasserin aut Enthalten in Journal of marine science and technology Tokyo : Springer, 1995 25(2019), 2 vom: 30. Mai, Seite 467-481 (DE-627)300185499 (DE-600)1481609-X 1437-8213 nnns volume:25 year:2019 number:2 day:30 month:05 pages:467-481 https://dx.doi.org/10.1007/s00773-019-00654-z lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER SSG-OPC-GGO SSG-OPC-ASE GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_267 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2070 GBV_ILN_2086 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2116 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 38.90 ASE 50.92 ASE 38.48 ASE AR 25 2019 2 30 05 467-481
allfields_unstemmed	10.1007/s00773-019-00654-z doi (DE-627)SPR039766381 (SPR)s00773-019-00654-z-e DE-627 ger DE-627 rakwb eng 550 620 ASE 380 ASE 38.90 bkl 50.92 bkl 38.48 bkl Lou, Min verfasserin aut Experimental investigation of the suppression of vortex-induced vibration in four cylinders arranged in a square under different spacing ratios 2019 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract A vortex-induced vibration (VIV) is a typical flow-structure interference phenomenon that causes an unsteady flow pattern owing to vortex shedding at or near the structure’s natural frequency, leading to resonant vibrations. VIVs can cause the failure of marine risers owing to premature fatigue, because of which a growing amount of research has attended to them. To investigate the effects of suppressing the VIV of splitter plates on a square array of cylinders under different spacing ratios, cylinders undergoing VIV in a flow with a Reynolds number ranging from 3300 to 6750 were experimentally studied in this paper. The results show that the splitter plate can suppress cross-flow (CF) vibrations as well as in-line flow (IF) vibrations in the cylinders. For cross-flow vibration, the suppression effects of the splitter plate on the upstream cylinders were at their maximum at %$S/D = 5%$ while the effects on downstream cylinders reached this at %$S/D = 6%$, where %$S/D%$ refers to the ratio of the distance between the centers of cylinders to its diameter. For in-line flow vibrations, the effects on upstream and downstream cylinders all reached the maximum at %$S/D = 4%$. The vibrational frequency of the cylinder with splitter plate was also lower than that of the bare cylinder in the flow. Vortex-induced vibration (dpeaa)DE-He213 Suppression (dpeaa)DE-He213 Splitter plates (dpeaa)DE-He213 Square arrangement (dpeaa)DE-He213 Spacing ratio (dpeaa)DE-He213 Qian, Gang verfasserin aut Li, Run verfasserin aut Enthalten in Journal of marine science and technology Tokyo : Springer, 1995 25(2019), 2 vom: 30. Mai, Seite 467-481 (DE-627)300185499 (DE-600)1481609-X 1437-8213 nnns volume:25 year:2019 number:2 day:30 month:05 pages:467-481 https://dx.doi.org/10.1007/s00773-019-00654-z lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER SSG-OPC-GGO SSG-OPC-ASE GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_267 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2070 GBV_ILN_2086 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2116 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 38.90 ASE 50.92 ASE 38.48 ASE AR 25 2019 2 30 05 467-481
allfieldsGer	10.1007/s00773-019-00654-z doi (DE-627)SPR039766381 (SPR)s00773-019-00654-z-e DE-627 ger DE-627 rakwb eng 550 620 ASE 380 ASE 38.90 bkl 50.92 bkl 38.48 bkl Lou, Min verfasserin aut Experimental investigation of the suppression of vortex-induced vibration in four cylinders arranged in a square under different spacing ratios 2019 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract A vortex-induced vibration (VIV) is a typical flow-structure interference phenomenon that causes an unsteady flow pattern owing to vortex shedding at or near the structure’s natural frequency, leading to resonant vibrations. VIVs can cause the failure of marine risers owing to premature fatigue, because of which a growing amount of research has attended to them. To investigate the effects of suppressing the VIV of splitter plates on a square array of cylinders under different spacing ratios, cylinders undergoing VIV in a flow with a Reynolds number ranging from 3300 to 6750 were experimentally studied in this paper. The results show that the splitter plate can suppress cross-flow (CF) vibrations as well as in-line flow (IF) vibrations in the cylinders. For cross-flow vibration, the suppression effects of the splitter plate on the upstream cylinders were at their maximum at %$S/D = 5%$ while the effects on downstream cylinders reached this at %$S/D = 6%$, where %$S/D%$ refers to the ratio of the distance between the centers of cylinders to its diameter. For in-line flow vibrations, the effects on upstream and downstream cylinders all reached the maximum at %$S/D = 4%$. The vibrational frequency of the cylinder with splitter plate was also lower than that of the bare cylinder in the flow. Vortex-induced vibration (dpeaa)DE-He213 Suppression (dpeaa)DE-He213 Splitter plates (dpeaa)DE-He213 Square arrangement (dpeaa)DE-He213 Spacing ratio (dpeaa)DE-He213 Qian, Gang verfasserin aut Li, Run verfasserin aut Enthalten in Journal of marine science and technology Tokyo : Springer, 1995 25(2019), 2 vom: 30. Mai, Seite 467-481 (DE-627)300185499 (DE-600)1481609-X 1437-8213 nnns volume:25 year:2019 number:2 day:30 month:05 pages:467-481 https://dx.doi.org/10.1007/s00773-019-00654-z lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER SSG-OPC-GGO SSG-OPC-ASE GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_267 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2070 GBV_ILN_2086 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2116 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 38.90 ASE 50.92 ASE 38.48 ASE AR 25 2019 2 30 05 467-481
allfieldsSound	10.1007/s00773-019-00654-z doi (DE-627)SPR039766381 (SPR)s00773-019-00654-z-e DE-627 ger DE-627 rakwb eng 550 620 ASE 380 ASE 38.90 bkl 50.92 bkl 38.48 bkl Lou, Min verfasserin aut Experimental investigation of the suppression of vortex-induced vibration in four cylinders arranged in a square under different spacing ratios 2019 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract A vortex-induced vibration (VIV) is a typical flow-structure interference phenomenon that causes an unsteady flow pattern owing to vortex shedding at or near the structure’s natural frequency, leading to resonant vibrations. VIVs can cause the failure of marine risers owing to premature fatigue, because of which a growing amount of research has attended to them. To investigate the effects of suppressing the VIV of splitter plates on a square array of cylinders under different spacing ratios, cylinders undergoing VIV in a flow with a Reynolds number ranging from 3300 to 6750 were experimentally studied in this paper. The results show that the splitter plate can suppress cross-flow (CF) vibrations as well as in-line flow (IF) vibrations in the cylinders. For cross-flow vibration, the suppression effects of the splitter plate on the upstream cylinders were at their maximum at %$S/D = 5%$ while the effects on downstream cylinders reached this at %$S/D = 6%$, where %$S/D%$ refers to the ratio of the distance between the centers of cylinders to its diameter. For in-line flow vibrations, the effects on upstream and downstream cylinders all reached the maximum at %$S/D = 4%$. The vibrational frequency of the cylinder with splitter plate was also lower than that of the bare cylinder in the flow. Vortex-induced vibration (dpeaa)DE-He213 Suppression (dpeaa)DE-He213 Splitter plates (dpeaa)DE-He213 Square arrangement (dpeaa)DE-He213 Spacing ratio (dpeaa)DE-He213 Qian, Gang verfasserin aut Li, Run verfasserin aut Enthalten in Journal of marine science and technology Tokyo : Springer, 1995 25(2019), 2 vom: 30. Mai, Seite 467-481 (DE-627)300185499 (DE-600)1481609-X 1437-8213 nnns volume:25 year:2019 number:2 day:30 month:05 pages:467-481 https://dx.doi.org/10.1007/s00773-019-00654-z lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER SSG-OPC-GGO SSG-OPC-ASE GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_267 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2070 GBV_ILN_2086 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2116 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 38.90 ASE 50.92 ASE 38.48 ASE AR 25 2019 2 30 05 467-481
language	English
source	Enthalten in Journal of marine science and technology 25(2019), 2 vom: 30. Mai, Seite 467-481 volume:25 year:2019 number:2 day:30 month:05 pages:467-481
sourceStr	Enthalten in Journal of marine science and technology 25(2019), 2 vom: 30. Mai, Seite 467-481 volume:25 year:2019 number:2 day:30 month:05 pages:467-481
format_phy_str_mv	Article
institution	findex.gbv.de
topic_facet	Vortex-induced vibration Suppression Splitter plates Square arrangement Spacing ratio
dewey-raw	550
isfreeaccess_bool	false
container_title	Journal of marine science and technology
authorswithroles_txt_mv	Lou, Min @@aut@@ Qian, Gang @@aut@@ Li, Run @@aut@@
publishDateDaySort_date	2019-05-30T00:00:00Z
hierarchy_top_id	300185499
dewey-sort	3550
id	SPR039766381
language_de	englisch
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author	Lou, Min
spellingShingle	Lou, Min ddc 550 ddc 380 bkl 38.90 bkl 50.92 bkl 38.48 misc Vortex-induced vibration misc Suppression misc Splitter plates misc Square arrangement misc Spacing ratio Experimental investigation of the suppression of vortex-induced vibration in four cylinders arranged in a square under different spacing ratios
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topic_title	550 620 ASE 380 ASE 38.90 bkl 50.92 bkl 38.48 bkl Experimental investigation of the suppression of vortex-induced vibration in four cylinders arranged in a square under different spacing ratios Vortex-induced vibration (dpeaa)DE-He213 Suppression (dpeaa)DE-He213 Splitter plates (dpeaa)DE-He213 Square arrangement (dpeaa)DE-He213 Spacing ratio (dpeaa)DE-He213
topic	ddc 550 ddc 380 bkl 38.90 bkl 50.92 bkl 38.48 misc Vortex-induced vibration misc Suppression misc Splitter plates misc Square arrangement misc Spacing ratio
topic_unstemmed	ddc 550 ddc 380 bkl 38.90 bkl 50.92 bkl 38.48 misc Vortex-induced vibration misc Suppression misc Splitter plates misc Square arrangement misc Spacing ratio
topic_browse	ddc 550 ddc 380 bkl 38.90 bkl 50.92 bkl 38.48 misc Vortex-induced vibration misc Suppression misc Splitter plates misc Square arrangement misc Spacing ratio
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title	Experimental investigation of the suppression of vortex-induced vibration in four cylinders arranged in a square under different spacing ratios
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title_full	Experimental investigation of the suppression of vortex-induced vibration in four cylinders arranged in a square under different spacing ratios
author_sort	Lou, Min
journal	Journal of marine science and technology
journalStr	Journal of marine science and technology
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author_browse	Lou, Min Qian, Gang Li, Run
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class	550 620 ASE 380 ASE 38.90 bkl 50.92 bkl 38.48 bkl
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author-letter	Lou, Min
doi_str_mv	10.1007/s00773-019-00654-z
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title_sort	experimental investigation of the suppression of vortex-induced vibration in four cylinders arranged in a square under different spacing ratios
title_auth	Experimental investigation of the suppression of vortex-induced vibration in four cylinders arranged in a square under different spacing ratios
abstract	Abstract A vortex-induced vibration (VIV) is a typical flow-structure interference phenomenon that causes an unsteady flow pattern owing to vortex shedding at or near the structure’s natural frequency, leading to resonant vibrations. VIVs can cause the failure of marine risers owing to premature fatigue, because of which a growing amount of research has attended to them. To investigate the effects of suppressing the VIV of splitter plates on a square array of cylinders under different spacing ratios, cylinders undergoing VIV in a flow with a Reynolds number ranging from 3300 to 6750 were experimentally studied in this paper. The results show that the splitter plate can suppress cross-flow (CF) vibrations as well as in-line flow (IF) vibrations in the cylinders. For cross-flow vibration, the suppression effects of the splitter plate on the upstream cylinders were at their maximum at %$S/D = 5%$ while the effects on downstream cylinders reached this at %$S/D = 6%$, where %$S/D%$ refers to the ratio of the distance between the centers of cylinders to its diameter. For in-line flow vibrations, the effects on upstream and downstream cylinders all reached the maximum at %$S/D = 4%$. The vibrational frequency of the cylinder with splitter plate was also lower than that of the bare cylinder in the flow.
abstractGer	Abstract A vortex-induced vibration (VIV) is a typical flow-structure interference phenomenon that causes an unsteady flow pattern owing to vortex shedding at or near the structure’s natural frequency, leading to resonant vibrations. VIVs can cause the failure of marine risers owing to premature fatigue, because of which a growing amount of research has attended to them. To investigate the effects of suppressing the VIV of splitter plates on a square array of cylinders under different spacing ratios, cylinders undergoing VIV in a flow with a Reynolds number ranging from 3300 to 6750 were experimentally studied in this paper. The results show that the splitter plate can suppress cross-flow (CF) vibrations as well as in-line flow (IF) vibrations in the cylinders. For cross-flow vibration, the suppression effects of the splitter plate on the upstream cylinders were at their maximum at %$S/D = 5%$ while the effects on downstream cylinders reached this at %$S/D = 6%$, where %$S/D%$ refers to the ratio of the distance between the centers of cylinders to its diameter. For in-line flow vibrations, the effects on upstream and downstream cylinders all reached the maximum at %$S/D = 4%$. The vibrational frequency of the cylinder with splitter plate was also lower than that of the bare cylinder in the flow.
abstract_unstemmed	Abstract A vortex-induced vibration (VIV) is a typical flow-structure interference phenomenon that causes an unsteady flow pattern owing to vortex shedding at or near the structure’s natural frequency, leading to resonant vibrations. VIVs can cause the failure of marine risers owing to premature fatigue, because of which a growing amount of research has attended to them. To investigate the effects of suppressing the VIV of splitter plates on a square array of cylinders under different spacing ratios, cylinders undergoing VIV in a flow with a Reynolds number ranging from 3300 to 6750 were experimentally studied in this paper. The results show that the splitter plate can suppress cross-flow (CF) vibrations as well as in-line flow (IF) vibrations in the cylinders. For cross-flow vibration, the suppression effects of the splitter plate on the upstream cylinders were at their maximum at %$S/D = 5%$ while the effects on downstream cylinders reached this at %$S/D = 6%$, where %$S/D%$ refers to the ratio of the distance between the centers of cylinders to its diameter. For in-line flow vibrations, the effects on upstream and downstream cylinders all reached the maximum at %$S/D = 4%$. The vibrational frequency of the cylinder with splitter plate was also lower than that of the bare cylinder in the flow.
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title_short	Experimental investigation of the suppression of vortex-induced vibration in four cylinders arranged in a square under different spacing ratios
url	https://dx.doi.org/10.1007/s00773-019-00654-z
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author2	Qian, Gang Li, Run
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doi_str	10.1007/s00773-019-00654-z
up_date	2024-07-04T01:28:16.223Z
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fullrecord_marcxml	<?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01000caa a22002652 4500</leader><controlfield tag="001">SPR039766381</controlfield><controlfield tag="003">DE-627</controlfield><controlfield tag="005">20220110195518.0</controlfield><controlfield tag="007">cr uuu---uuuuu</controlfield><controlfield tag="008">201007s2019 xx \|\|\|\|\|o 00\| \|\|eng c</controlfield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.1007/s00773-019-00654-z</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-627)SPR039766381</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(SPR)s00773-019-00654-z-e</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-627</subfield><subfield code="b">ger</subfield><subfield code="c">DE-627</subfield><subfield code="e">rakwb</subfield></datafield><datafield tag="041" ind1=" " ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="082" ind1="0" ind2="4"><subfield code="a">550</subfield><subfield code="a">620</subfield><subfield code="q">ASE</subfield></datafield><datafield tag="082" ind1="0" ind2="4"><subfield code="a">380</subfield><subfield code="q">ASE</subfield></datafield><datafield tag="084" ind1=" " ind2=" "><subfield code="a">38.90</subfield><subfield code="2">bkl</subfield></datafield><datafield tag="084" ind1=" " ind2=" "><subfield code="a">50.92</subfield><subfield code="2">bkl</subfield></datafield><datafield tag="084" ind1=" " ind2=" "><subfield code="a">38.48</subfield><subfield code="2">bkl</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Lou, Min</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Experimental investigation of the suppression of vortex-induced vibration in four cylinders arranged in a square under different spacing ratios</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">2019</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="a">Text</subfield><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="a">Computermedien</subfield><subfield code="b">c</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">Online-Ressource</subfield><subfield code="b">cr</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Abstract A vortex-induced vibration (VIV) is a typical flow-structure interference phenomenon that causes an unsteady flow pattern owing to vortex shedding at or near the structure’s natural frequency, leading to resonant vibrations. VIVs can cause the failure of marine risers owing to premature fatigue, because of which a growing amount of research has attended to them. To investigate the effects of suppressing the VIV of splitter plates on a square array of cylinders under different spacing ratios, cylinders undergoing VIV in a flow with a Reynolds number ranging from 3300 to 6750 were experimentally studied in this paper. The results show that the splitter plate can suppress cross-flow (CF) vibrations as well as in-line flow (IF) vibrations in the cylinders. For cross-flow vibration, the suppression effects of the splitter plate on the upstream cylinders were at their maximum at %$S/D = 5%$ while the effects on downstream cylinders reached this at %$S/D = 6%$, where %$S/D%$ refers to the ratio of the distance between the centers of cylinders to its diameter. For in-line flow vibrations, the effects on upstream and downstream cylinders all reached the maximum at %$S/D = 4%$. 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Experimental investigation of the suppression of vortex-induced vibration in four cylinders arranged in a square under different spacing ratios

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