Experimental Investigation and Large-Eddy Simulation of the Turbulent Flow past a Smooth and Rigid Hemisphere

Abstract The objective of the present paper is to provide a detailed experimental and numerical investigation on the turbulent flow past a hemispherical obstacle (diameter D). For this purpose, the bluff body is exposed to a thick turbulent boundary layer of the thickness δ = D/2 at Re = 50,000. In...
Ausführliche Beschreibung

Gespeichert in:

Autor*in:	Wood, Jens Nikolas [verfasserIn] De Nayer, Guillaume [verfasserIn] Schmidt, Stephan [verfasserIn] Breuer, Michael [verfasserIn]

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2016

Schlagwörter:	Hemisphere Hemispherical dome Turbulent flow Laser-Doppler anemometry Constant temperature anemometry Large-eddy simulation (LES) Wind load Artificial boundary layer Inflow generator

Übergeordnetes Werk:	Enthalten in: Flow, turbulence and combustion - Dordrecht [u.a.] : Springer Science + Business Media B.V., 1947, 97(2016), 1 vom: 11. Jan., Seite 79-119
Übergeordnetes Werk:	volume:97 ; year:2016 ; number:1 ; day:11 ; month:01 ; pages:79-119

Links:	Volltext

DOI / URN:	10.1007/s10494-015-9690-5

Katalog-ID:	SPR010484469

Internformat


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520			\|a Abstract The objective of the present paper is to provide a detailed experimental and numerical investigation on the turbulent flow past a hemispherical obstacle (diameter D). For this purpose, the bluff body is exposed to a thick turbulent boundary layer of the thickness δ = D/2 at Re = 50,000. In the experiment this boundary layer thickness is achieved by specific fences placed in the upstream region of the wind tunnel. A detailed measurement of the upstream flow conditions by laser-Doppler and hot-film probes allows to mimic the inflow conditions for the complementary large-eddy simulation of the flow field using a synthetic turbulence inflow generator. These clearly defined boundary and operating conditions are the prerequisites for a combined experimental and numerical investigation of the flow field relying on the laser-Doppler anemometry and a finite-volume Navier-Stokes solver for block-structured curvilinear grids. The results comprise an analysis on the unsteady flow features observed in the vicinity of the hemisphere as well as a detailed discussion of the time-averaged flow field. The latter includes the mean velocity field as well as the Reynolds stresses. Owing to the proper description of the oncoming flow and supplementary numerical studies guaranteeing the choice of an appropriate grid and subgrid-scale model, the results of the measurements and the prediction are found to be in close agreement.
650		4	\|a Hemisphere \|7 (dpeaa)DE-He213
650		4	\|a Hemispherical dome \|7 (dpeaa)DE-He213
650		4	\|a Turbulent flow \|7 (dpeaa)DE-He213
650		4	\|a Laser-Doppler anemometry \|7 (dpeaa)DE-He213
650		4	\|a Constant temperature anemometry \|7 (dpeaa)DE-He213
650		4	\|a Large-eddy simulation (LES) \|7 (dpeaa)DE-He213
650		4	\|a Wind load \|7 (dpeaa)DE-He213
650		4	\|a Artificial boundary layer \|7 (dpeaa)DE-He213
650		4	\|a Inflow generator \|7 (dpeaa)DE-He213
700	1		\|a De Nayer, Guillaume \|e verfasserin \|4 aut
700	1		\|a Schmidt, Stephan \|e verfasserin \|4 aut
700	1		\|a Breuer, Michael \|e verfasserin \|4 aut
773	0	8	\|i Enthalten in \|t Flow, turbulence and combustion \|d Dordrecht [u.a.] : Springer Science + Business Media B.V., 1947 \|g 97(2016), 1 vom: 11. Jan., Seite 79-119 \|w (DE-627)302722408 \|w (DE-600)1492282-4 \|x 1573-1987 \|7 nnns
773	1	8	\|g volume:97 \|g year:2016 \|g number:1 \|g day:11 \|g month:01 \|g pages:79-119
856	4	0	\|u https://dx.doi.org/10.1007/s10494-015-9690-5 \|z lizenzpflichtig \|3 Volltext
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952			\|d 97 \|j 2016 \|e 1 \|b 11 \|c 01 \|h 79-119

Indexfelder

author_variant	j n w jn jnw n g d ng ngd s s ss m b mb
matchkey_str	article:15731987:2016----::xeietlnetgtoadagedsmltooteublnfops
hierarchy_sort_str	2016
bklnumber	50.34 52.51
publishDate	2016
allfields	10.1007/s10494-015-9690-5 doi (DE-627)SPR010484469 (SPR)s10494-015-9690-5-e DE-627 ger DE-627 rakwb eng 500 600 ASE 50.34 bkl 52.51 bkl Wood, Jens Nikolas verfasserin aut Experimental Investigation and Large-Eddy Simulation of the Turbulent Flow past a Smooth and Rigid Hemisphere 2016 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract The objective of the present paper is to provide a detailed experimental and numerical investigation on the turbulent flow past a hemispherical obstacle (diameter D). For this purpose, the bluff body is exposed to a thick turbulent boundary layer of the thickness δ = D/2 at Re = 50,000. In the experiment this boundary layer thickness is achieved by specific fences placed in the upstream region of the wind tunnel. A detailed measurement of the upstream flow conditions by laser-Doppler and hot-film probes allows to mimic the inflow conditions for the complementary large-eddy simulation of the flow field using a synthetic turbulence inflow generator. These clearly defined boundary and operating conditions are the prerequisites for a combined experimental and numerical investigation of the flow field relying on the laser-Doppler anemometry and a finite-volume Navier-Stokes solver for block-structured curvilinear grids. The results comprise an analysis on the unsteady flow features observed in the vicinity of the hemisphere as well as a detailed discussion of the time-averaged flow field. The latter includes the mean velocity field as well as the Reynolds stresses. Owing to the proper description of the oncoming flow and supplementary numerical studies guaranteeing the choice of an appropriate grid and subgrid-scale model, the results of the measurements and the prediction are found to be in close agreement. Hemisphere (dpeaa)DE-He213 Hemispherical dome (dpeaa)DE-He213 Turbulent flow (dpeaa)DE-He213 Laser-Doppler anemometry (dpeaa)DE-He213 Constant temperature anemometry (dpeaa)DE-He213 Large-eddy simulation (LES) (dpeaa)DE-He213 Wind load (dpeaa)DE-He213 Artificial boundary layer (dpeaa)DE-He213 Inflow generator (dpeaa)DE-He213 De Nayer, Guillaume verfasserin aut Schmidt, Stephan verfasserin aut Breuer, Michael verfasserin aut Enthalten in Flow, turbulence and combustion Dordrecht [u.a.] : Springer Science + Business Media B.V., 1947 97(2016), 1 vom: 11. Jan., Seite 79-119 (DE-627)302722408 (DE-600)1492282-4 1573-1987 nnns volume:97 year:2016 number:1 day:11 month:01 pages:79-119 https://dx.doi.org/10.1007/s10494-015-9690-5 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER 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_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_2008 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_4012 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 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 50.34 ASE 52.51 ASE AR 97 2016 1 11 01 79-119
spelling	10.1007/s10494-015-9690-5 doi (DE-627)SPR010484469 (SPR)s10494-015-9690-5-e DE-627 ger DE-627 rakwb eng 500 600 ASE 50.34 bkl 52.51 bkl Wood, Jens Nikolas verfasserin aut Experimental Investigation and Large-Eddy Simulation of the Turbulent Flow past a Smooth and Rigid Hemisphere 2016 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract The objective of the present paper is to provide a detailed experimental and numerical investigation on the turbulent flow past a hemispherical obstacle (diameter D). For this purpose, the bluff body is exposed to a thick turbulent boundary layer of the thickness δ = D/2 at Re = 50,000. In the experiment this boundary layer thickness is achieved by specific fences placed in the upstream region of the wind tunnel. A detailed measurement of the upstream flow conditions by laser-Doppler and hot-film probes allows to mimic the inflow conditions for the complementary large-eddy simulation of the flow field using a synthetic turbulence inflow generator. These clearly defined boundary and operating conditions are the prerequisites for a combined experimental and numerical investigation of the flow field relying on the laser-Doppler anemometry and a finite-volume Navier-Stokes solver for block-structured curvilinear grids. The results comprise an analysis on the unsteady flow features observed in the vicinity of the hemisphere as well as a detailed discussion of the time-averaged flow field. The latter includes the mean velocity field as well as the Reynolds stresses. Owing to the proper description of the oncoming flow and supplementary numerical studies guaranteeing the choice of an appropriate grid and subgrid-scale model, the results of the measurements and the prediction are found to be in close agreement. Hemisphere (dpeaa)DE-He213 Hemispherical dome (dpeaa)DE-He213 Turbulent flow (dpeaa)DE-He213 Laser-Doppler anemometry (dpeaa)DE-He213 Constant temperature anemometry (dpeaa)DE-He213 Large-eddy simulation (LES) (dpeaa)DE-He213 Wind load (dpeaa)DE-He213 Artificial boundary layer (dpeaa)DE-He213 Inflow generator (dpeaa)DE-He213 De Nayer, Guillaume verfasserin aut Schmidt, Stephan verfasserin aut Breuer, Michael verfasserin aut Enthalten in Flow, turbulence and combustion Dordrecht [u.a.] : Springer Science + Business Media B.V., 1947 97(2016), 1 vom: 11. Jan., Seite 79-119 (DE-627)302722408 (DE-600)1492282-4 1573-1987 nnns volume:97 year:2016 number:1 day:11 month:01 pages:79-119 https://dx.doi.org/10.1007/s10494-015-9690-5 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER 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_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_2008 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_4012 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 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 50.34 ASE 52.51 ASE AR 97 2016 1 11 01 79-119
allfields_unstemmed	10.1007/s10494-015-9690-5 doi (DE-627)SPR010484469 (SPR)s10494-015-9690-5-e DE-627 ger DE-627 rakwb eng 500 600 ASE 50.34 bkl 52.51 bkl Wood, Jens Nikolas verfasserin aut Experimental Investigation and Large-Eddy Simulation of the Turbulent Flow past a Smooth and Rigid Hemisphere 2016 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract The objective of the present paper is to provide a detailed experimental and numerical investigation on the turbulent flow past a hemispherical obstacle (diameter D). For this purpose, the bluff body is exposed to a thick turbulent boundary layer of the thickness δ = D/2 at Re = 50,000. In the experiment this boundary layer thickness is achieved by specific fences placed in the upstream region of the wind tunnel. A detailed measurement of the upstream flow conditions by laser-Doppler and hot-film probes allows to mimic the inflow conditions for the complementary large-eddy simulation of the flow field using a synthetic turbulence inflow generator. These clearly defined boundary and operating conditions are the prerequisites for a combined experimental and numerical investigation of the flow field relying on the laser-Doppler anemometry and a finite-volume Navier-Stokes solver for block-structured curvilinear grids. The results comprise an analysis on the unsteady flow features observed in the vicinity of the hemisphere as well as a detailed discussion of the time-averaged flow field. The latter includes the mean velocity field as well as the Reynolds stresses. Owing to the proper description of the oncoming flow and supplementary numerical studies guaranteeing the choice of an appropriate grid and subgrid-scale model, the results of the measurements and the prediction are found to be in close agreement. Hemisphere (dpeaa)DE-He213 Hemispherical dome (dpeaa)DE-He213 Turbulent flow (dpeaa)DE-He213 Laser-Doppler anemometry (dpeaa)DE-He213 Constant temperature anemometry (dpeaa)DE-He213 Large-eddy simulation (LES) (dpeaa)DE-He213 Wind load (dpeaa)DE-He213 Artificial boundary layer (dpeaa)DE-He213 Inflow generator (dpeaa)DE-He213 De Nayer, Guillaume verfasserin aut Schmidt, Stephan verfasserin aut Breuer, Michael verfasserin aut Enthalten in Flow, turbulence and combustion Dordrecht [u.a.] : Springer Science + Business Media B.V., 1947 97(2016), 1 vom: 11. Jan., Seite 79-119 (DE-627)302722408 (DE-600)1492282-4 1573-1987 nnns volume:97 year:2016 number:1 day:11 month:01 pages:79-119 https://dx.doi.org/10.1007/s10494-015-9690-5 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER 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_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_2008 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_4012 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 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 50.34 ASE 52.51 ASE AR 97 2016 1 11 01 79-119
allfieldsGer	10.1007/s10494-015-9690-5 doi (DE-627)SPR010484469 (SPR)s10494-015-9690-5-e DE-627 ger DE-627 rakwb eng 500 600 ASE 50.34 bkl 52.51 bkl Wood, Jens Nikolas verfasserin aut Experimental Investigation and Large-Eddy Simulation of the Turbulent Flow past a Smooth and Rigid Hemisphere 2016 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract The objective of the present paper is to provide a detailed experimental and numerical investigation on the turbulent flow past a hemispherical obstacle (diameter D). For this purpose, the bluff body is exposed to a thick turbulent boundary layer of the thickness δ = D/2 at Re = 50,000. In the experiment this boundary layer thickness is achieved by specific fences placed in the upstream region of the wind tunnel. A detailed measurement of the upstream flow conditions by laser-Doppler and hot-film probes allows to mimic the inflow conditions for the complementary large-eddy simulation of the flow field using a synthetic turbulence inflow generator. These clearly defined boundary and operating conditions are the prerequisites for a combined experimental and numerical investigation of the flow field relying on the laser-Doppler anemometry and a finite-volume Navier-Stokes solver for block-structured curvilinear grids. The results comprise an analysis on the unsteady flow features observed in the vicinity of the hemisphere as well as a detailed discussion of the time-averaged flow field. The latter includes the mean velocity field as well as the Reynolds stresses. Owing to the proper description of the oncoming flow and supplementary numerical studies guaranteeing the choice of an appropriate grid and subgrid-scale model, the results of the measurements and the prediction are found to be in close agreement. Hemisphere (dpeaa)DE-He213 Hemispherical dome (dpeaa)DE-He213 Turbulent flow (dpeaa)DE-He213 Laser-Doppler anemometry (dpeaa)DE-He213 Constant temperature anemometry (dpeaa)DE-He213 Large-eddy simulation (LES) (dpeaa)DE-He213 Wind load (dpeaa)DE-He213 Artificial boundary layer (dpeaa)DE-He213 Inflow generator (dpeaa)DE-He213 De Nayer, Guillaume verfasserin aut Schmidt, Stephan verfasserin aut Breuer, Michael verfasserin aut Enthalten in Flow, turbulence and combustion Dordrecht [u.a.] : Springer Science + Business Media B.V., 1947 97(2016), 1 vom: 11. Jan., Seite 79-119 (DE-627)302722408 (DE-600)1492282-4 1573-1987 nnns volume:97 year:2016 number:1 day:11 month:01 pages:79-119 https://dx.doi.org/10.1007/s10494-015-9690-5 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER 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_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_2008 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_4012 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 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 50.34 ASE 52.51 ASE AR 97 2016 1 11 01 79-119
allfieldsSound	10.1007/s10494-015-9690-5 doi (DE-627)SPR010484469 (SPR)s10494-015-9690-5-e DE-627 ger DE-627 rakwb eng 500 600 ASE 50.34 bkl 52.51 bkl Wood, Jens Nikolas verfasserin aut Experimental Investigation and Large-Eddy Simulation of the Turbulent Flow past a Smooth and Rigid Hemisphere 2016 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract The objective of the present paper is to provide a detailed experimental and numerical investigation on the turbulent flow past a hemispherical obstacle (diameter D). For this purpose, the bluff body is exposed to a thick turbulent boundary layer of the thickness δ = D/2 at Re = 50,000. In the experiment this boundary layer thickness is achieved by specific fences placed in the upstream region of the wind tunnel. A detailed measurement of the upstream flow conditions by laser-Doppler and hot-film probes allows to mimic the inflow conditions for the complementary large-eddy simulation of the flow field using a synthetic turbulence inflow generator. These clearly defined boundary and operating conditions are the prerequisites for a combined experimental and numerical investigation of the flow field relying on the laser-Doppler anemometry and a finite-volume Navier-Stokes solver for block-structured curvilinear grids. The results comprise an analysis on the unsteady flow features observed in the vicinity of the hemisphere as well as a detailed discussion of the time-averaged flow field. The latter includes the mean velocity field as well as the Reynolds stresses. Owing to the proper description of the oncoming flow and supplementary numerical studies guaranteeing the choice of an appropriate grid and subgrid-scale model, the results of the measurements and the prediction are found to be in close agreement. Hemisphere (dpeaa)DE-He213 Hemispherical dome (dpeaa)DE-He213 Turbulent flow (dpeaa)DE-He213 Laser-Doppler anemometry (dpeaa)DE-He213 Constant temperature anemometry (dpeaa)DE-He213 Large-eddy simulation (LES) (dpeaa)DE-He213 Wind load (dpeaa)DE-He213 Artificial boundary layer (dpeaa)DE-He213 Inflow generator (dpeaa)DE-He213 De Nayer, Guillaume verfasserin aut Schmidt, Stephan verfasserin aut Breuer, Michael verfasserin aut Enthalten in Flow, turbulence and combustion Dordrecht [u.a.] : Springer Science + Business Media B.V., 1947 97(2016), 1 vom: 11. Jan., Seite 79-119 (DE-627)302722408 (DE-600)1492282-4 1573-1987 nnns volume:97 year:2016 number:1 day:11 month:01 pages:79-119 https://dx.doi.org/10.1007/s10494-015-9690-5 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER 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_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_2008 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_4012 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 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 50.34 ASE 52.51 ASE AR 97 2016 1 11 01 79-119
language	English
source	Enthalten in Flow, turbulence and combustion 97(2016), 1 vom: 11. Jan., Seite 79-119 volume:97 year:2016 number:1 day:11 month:01 pages:79-119
sourceStr	Enthalten in Flow, turbulence and combustion 97(2016), 1 vom: 11. Jan., Seite 79-119 volume:97 year:2016 number:1 day:11 month:01 pages:79-119
format_phy_str_mv	Article
institution	findex.gbv.de
topic_facet	Hemisphere Hemispherical dome Turbulent flow Laser-Doppler anemometry Constant temperature anemometry Large-eddy simulation (LES) Wind load Artificial boundary layer Inflow generator
dewey-raw	500
isfreeaccess_bool	false
container_title	Flow, turbulence and combustion
authorswithroles_txt_mv	Wood, Jens Nikolas @@aut@@ De Nayer, Guillaume @@aut@@ Schmidt, Stephan @@aut@@ Breuer, Michael @@aut@@
publishDateDaySort_date	2016-01-11T00:00:00Z
hierarchy_top_id	302722408
dewey-sort	3500
id	SPR010484469
language_de	englisch
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author	Wood, Jens Nikolas
spellingShingle	Wood, Jens Nikolas ddc 500 bkl 50.34 bkl 52.51 misc Hemisphere misc Hemispherical dome misc Turbulent flow misc Laser-Doppler anemometry misc Constant temperature anemometry misc Large-eddy simulation (LES) misc Wind load misc Artificial boundary layer misc Inflow generator Experimental Investigation and Large-Eddy Simulation of the Turbulent Flow past a Smooth and Rigid Hemisphere
authorStr	Wood, Jens Nikolas
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topic_title	500 600 ASE 50.34 bkl 52.51 bkl Experimental Investigation and Large-Eddy Simulation of the Turbulent Flow past a Smooth and Rigid Hemisphere Hemisphere (dpeaa)DE-He213 Hemispherical dome (dpeaa)DE-He213 Turbulent flow (dpeaa)DE-He213 Laser-Doppler anemometry (dpeaa)DE-He213 Constant temperature anemometry (dpeaa)DE-He213 Large-eddy simulation (LES) (dpeaa)DE-He213 Wind load (dpeaa)DE-He213 Artificial boundary layer (dpeaa)DE-He213 Inflow generator (dpeaa)DE-He213
topic	ddc 500 bkl 50.34 bkl 52.51 misc Hemisphere misc Hemispherical dome misc Turbulent flow misc Laser-Doppler anemometry misc Constant temperature anemometry misc Large-eddy simulation (LES) misc Wind load misc Artificial boundary layer misc Inflow generator
topic_unstemmed	ddc 500 bkl 50.34 bkl 52.51 misc Hemisphere misc Hemispherical dome misc Turbulent flow misc Laser-Doppler anemometry misc Constant temperature anemometry misc Large-eddy simulation (LES) misc Wind load misc Artificial boundary layer misc Inflow generator
topic_browse	ddc 500 bkl 50.34 bkl 52.51 misc Hemisphere misc Hemispherical dome misc Turbulent flow misc Laser-Doppler anemometry misc Constant temperature anemometry misc Large-eddy simulation (LES) misc Wind load misc Artificial boundary layer misc Inflow generator
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hierarchy_parent_title	Flow, turbulence and combustion
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title	Experimental Investigation and Large-Eddy Simulation of the Turbulent Flow past a Smooth and Rigid Hemisphere
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title_full	Experimental Investigation and Large-Eddy Simulation of the Turbulent Flow past a Smooth and Rigid Hemisphere
author_sort	Wood, Jens Nikolas
journal	Flow, turbulence and combustion
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author_browse	Wood, Jens Nikolas De Nayer, Guillaume Schmidt, Stephan Breuer, Michael
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author-letter	Wood, Jens Nikolas
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title_sort	experimental investigation and large-eddy simulation of the turbulent flow past a smooth and rigid hemisphere
title_auth	Experimental Investigation and Large-Eddy Simulation of the Turbulent Flow past a Smooth and Rigid Hemisphere
abstract	Abstract The objective of the present paper is to provide a detailed experimental and numerical investigation on the turbulent flow past a hemispherical obstacle (diameter D). For this purpose, the bluff body is exposed to a thick turbulent boundary layer of the thickness δ = D/2 at Re = 50,000. In the experiment this boundary layer thickness is achieved by specific fences placed in the upstream region of the wind tunnel. A detailed measurement of the upstream flow conditions by laser-Doppler and hot-film probes allows to mimic the inflow conditions for the complementary large-eddy simulation of the flow field using a synthetic turbulence inflow generator. These clearly defined boundary and operating conditions are the prerequisites for a combined experimental and numerical investigation of the flow field relying on the laser-Doppler anemometry and a finite-volume Navier-Stokes solver for block-structured curvilinear grids. The results comprise an analysis on the unsteady flow features observed in the vicinity of the hemisphere as well as a detailed discussion of the time-averaged flow field. The latter includes the mean velocity field as well as the Reynolds stresses. Owing to the proper description of the oncoming flow and supplementary numerical studies guaranteeing the choice of an appropriate grid and subgrid-scale model, the results of the measurements and the prediction are found to be in close agreement.
abstractGer	Abstract The objective of the present paper is to provide a detailed experimental and numerical investigation on the turbulent flow past a hemispherical obstacle (diameter D). For this purpose, the bluff body is exposed to a thick turbulent boundary layer of the thickness δ = D/2 at Re = 50,000. In the experiment this boundary layer thickness is achieved by specific fences placed in the upstream region of the wind tunnel. A detailed measurement of the upstream flow conditions by laser-Doppler and hot-film probes allows to mimic the inflow conditions for the complementary large-eddy simulation of the flow field using a synthetic turbulence inflow generator. These clearly defined boundary and operating conditions are the prerequisites for a combined experimental and numerical investigation of the flow field relying on the laser-Doppler anemometry and a finite-volume Navier-Stokes solver for block-structured curvilinear grids. The results comprise an analysis on the unsteady flow features observed in the vicinity of the hemisphere as well as a detailed discussion of the time-averaged flow field. The latter includes the mean velocity field as well as the Reynolds stresses. Owing to the proper description of the oncoming flow and supplementary numerical studies guaranteeing the choice of an appropriate grid and subgrid-scale model, the results of the measurements and the prediction are found to be in close agreement.
abstract_unstemmed	Abstract The objective of the present paper is to provide a detailed experimental and numerical investigation on the turbulent flow past a hemispherical obstacle (diameter D). For this purpose, the bluff body is exposed to a thick turbulent boundary layer of the thickness δ = D/2 at Re = 50,000. In the experiment this boundary layer thickness is achieved by specific fences placed in the upstream region of the wind tunnel. A detailed measurement of the upstream flow conditions by laser-Doppler and hot-film probes allows to mimic the inflow conditions for the complementary large-eddy simulation of the flow field using a synthetic turbulence inflow generator. These clearly defined boundary and operating conditions are the prerequisites for a combined experimental and numerical investigation of the flow field relying on the laser-Doppler anemometry and a finite-volume Navier-Stokes solver for block-structured curvilinear grids. The results comprise an analysis on the unsteady flow features observed in the vicinity of the hemisphere as well as a detailed discussion of the time-averaged flow field. The latter includes the mean velocity field as well as the Reynolds stresses. Owing to the proper description of the oncoming flow and supplementary numerical studies guaranteeing the choice of an appropriate grid and subgrid-scale model, the results of the measurements and the prediction are found to be in close agreement.
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title_short	Experimental Investigation and Large-Eddy Simulation of the Turbulent Flow past a Smooth and Rigid Hemisphere
url	https://dx.doi.org/10.1007/s10494-015-9690-5
remote_bool	true
author2	De Nayer, Guillaume Schmidt, Stephan Breuer, Michael
author2Str	De Nayer, Guillaume Schmidt, Stephan Breuer, Michael
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doi_str	10.1007/s10494-015-9690-5
up_date	2024-07-03T16:24:43.062Z
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Experimental Investigation and Large-Eddy Simulation of the Turbulent Flow past a Smooth and Rigid Hemisphere

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