How to estimate the low wavenumber turbulence frequency spectrum

Abstract An estimate of the low wavenumber component of surface turbulence shear stress as a function of frequency has been obtained through measurements of the correlations of the longitudinal component of turbulence velocity made close to the surface at y+=7. The data were acquired in a fully-deve...
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Autor*in:	Kronauer, R. E. [verfasserIn] Hollis, P. G. Bullock, K. J. Lai, J. C. S.

Format:	Artikel
Sprache:	Englisch

Erschienen:	1997

Schlagwörter:	Reynolds Number Pipe Flow Pipe Diameter Turbulence Velocity Turbulence Shear

Anmerkung:	© Springer-Verlag Berlin Heidelberg 1997

Übergeordnetes Werk:	Enthalten in: Experiments in fluids - Springer-Verlag, 1983, 23(1997), 5 vom: Nov., Seite 353-360
Übergeordnetes Werk:	volume:23 ; year:1997 ; number:5 ; month:11 ; pages:353-360

Links:	Volltext

DOI / URN:	10.1007/s003480050122

Katalog-ID:	OLC2074334176

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allfields	10.1007/s003480050122 doi (DE-627)OLC2074334176 (DE-He213)s003480050122-p DE-627 ger DE-627 rakwb eng 620 530 VZ 530 VZ Kronauer, R. E. verfasserin aut How to estimate the low wavenumber turbulence frequency spectrum 1997 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer-Verlag Berlin Heidelberg 1997 Abstract An estimate of the low wavenumber component of surface turbulence shear stress as a function of frequency has been obtained through measurements of the correlations of the longitudinal component of turbulence velocity made close to the surface at y+=7. The data were acquired in a fully-developed turbulent pipe flow at a Reynolds number (based on centreline velocity and pipe diameter) of 268000, using two single hot-wire anemometer probes. A novel data analysis procedure has been introduced to establish the accuracy limits of the low wavenumber turbulence energy estimate for frequencies in the similarity regime of wall turbulence and the results are compared with other measurement techniques. Reynolds Number Pipe Flow Pipe Diameter Turbulence Velocity Turbulence Shear Hollis, P. G. aut Bullock, K. J. aut Lai, J. C. S. aut Enthalten in Experiments in fluids Springer-Verlag, 1983 23(1997), 5 vom: Nov., Seite 353-360 (DE-627)130443794 (DE-600)710083-8 (DE-576)015977404 0723-4864 nnns volume:23 year:1997 number:5 month:11 pages:353-360 https://doi.org/10.1007/s003480050122 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY GBV_ILN_11 GBV_ILN_21 GBV_ILN_32 GBV_ILN_40 GBV_ILN_62 GBV_ILN_65 GBV_ILN_70 GBV_ILN_170 GBV_ILN_185 GBV_ILN_2006 GBV_ILN_2012 GBV_ILN_2014 GBV_ILN_2016 GBV_ILN_2018 GBV_ILN_2020 GBV_ILN_4046 GBV_ILN_4277 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4700 AR 23 1997 5 11 353-360
spelling	10.1007/s003480050122 doi (DE-627)OLC2074334176 (DE-He213)s003480050122-p DE-627 ger DE-627 rakwb eng 620 530 VZ 530 VZ Kronauer, R. E. verfasserin aut How to estimate the low wavenumber turbulence frequency spectrum 1997 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer-Verlag Berlin Heidelberg 1997 Abstract An estimate of the low wavenumber component of surface turbulence shear stress as a function of frequency has been obtained through measurements of the correlations of the longitudinal component of turbulence velocity made close to the surface at y+=7. The data were acquired in a fully-developed turbulent pipe flow at a Reynolds number (based on centreline velocity and pipe diameter) of 268000, using two single hot-wire anemometer probes. A novel data analysis procedure has been introduced to establish the accuracy limits of the low wavenumber turbulence energy estimate for frequencies in the similarity regime of wall turbulence and the results are compared with other measurement techniques. Reynolds Number Pipe Flow Pipe Diameter Turbulence Velocity Turbulence Shear Hollis, P. G. aut Bullock, K. J. aut Lai, J. C. S. aut Enthalten in Experiments in fluids Springer-Verlag, 1983 23(1997), 5 vom: Nov., Seite 353-360 (DE-627)130443794 (DE-600)710083-8 (DE-576)015977404 0723-4864 nnns volume:23 year:1997 number:5 month:11 pages:353-360 https://doi.org/10.1007/s003480050122 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY GBV_ILN_11 GBV_ILN_21 GBV_ILN_32 GBV_ILN_40 GBV_ILN_62 GBV_ILN_65 GBV_ILN_70 GBV_ILN_170 GBV_ILN_185 GBV_ILN_2006 GBV_ILN_2012 GBV_ILN_2014 GBV_ILN_2016 GBV_ILN_2018 GBV_ILN_2020 GBV_ILN_4046 GBV_ILN_4277 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4700 AR 23 1997 5 11 353-360
allfields_unstemmed	10.1007/s003480050122 doi (DE-627)OLC2074334176 (DE-He213)s003480050122-p DE-627 ger DE-627 rakwb eng 620 530 VZ 530 VZ Kronauer, R. E. verfasserin aut How to estimate the low wavenumber turbulence frequency spectrum 1997 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer-Verlag Berlin Heidelberg 1997 Abstract An estimate of the low wavenumber component of surface turbulence shear stress as a function of frequency has been obtained through measurements of the correlations of the longitudinal component of turbulence velocity made close to the surface at y+=7. The data were acquired in a fully-developed turbulent pipe flow at a Reynolds number (based on centreline velocity and pipe diameter) of 268000, using two single hot-wire anemometer probes. A novel data analysis procedure has been introduced to establish the accuracy limits of the low wavenumber turbulence energy estimate for frequencies in the similarity regime of wall turbulence and the results are compared with other measurement techniques. Reynolds Number Pipe Flow Pipe Diameter Turbulence Velocity Turbulence Shear Hollis, P. G. aut Bullock, K. J. aut Lai, J. C. S. aut Enthalten in Experiments in fluids Springer-Verlag, 1983 23(1997), 5 vom: Nov., Seite 353-360 (DE-627)130443794 (DE-600)710083-8 (DE-576)015977404 0723-4864 nnns volume:23 year:1997 number:5 month:11 pages:353-360 https://doi.org/10.1007/s003480050122 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY GBV_ILN_11 GBV_ILN_21 GBV_ILN_32 GBV_ILN_40 GBV_ILN_62 GBV_ILN_65 GBV_ILN_70 GBV_ILN_170 GBV_ILN_185 GBV_ILN_2006 GBV_ILN_2012 GBV_ILN_2014 GBV_ILN_2016 GBV_ILN_2018 GBV_ILN_2020 GBV_ILN_4046 GBV_ILN_4277 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4700 AR 23 1997 5 11 353-360
allfieldsGer	10.1007/s003480050122 doi (DE-627)OLC2074334176 (DE-He213)s003480050122-p DE-627 ger DE-627 rakwb eng 620 530 VZ 530 VZ Kronauer, R. E. verfasserin aut How to estimate the low wavenumber turbulence frequency spectrum 1997 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer-Verlag Berlin Heidelberg 1997 Abstract An estimate of the low wavenumber component of surface turbulence shear stress as a function of frequency has been obtained through measurements of the correlations of the longitudinal component of turbulence velocity made close to the surface at y+=7. The data were acquired in a fully-developed turbulent pipe flow at a Reynolds number (based on centreline velocity and pipe diameter) of 268000, using two single hot-wire anemometer probes. A novel data analysis procedure has been introduced to establish the accuracy limits of the low wavenumber turbulence energy estimate for frequencies in the similarity regime of wall turbulence and the results are compared with other measurement techniques. Reynolds Number Pipe Flow Pipe Diameter Turbulence Velocity Turbulence Shear Hollis, P. G. aut Bullock, K. J. aut Lai, J. C. S. aut Enthalten in Experiments in fluids Springer-Verlag, 1983 23(1997), 5 vom: Nov., Seite 353-360 (DE-627)130443794 (DE-600)710083-8 (DE-576)015977404 0723-4864 nnns volume:23 year:1997 number:5 month:11 pages:353-360 https://doi.org/10.1007/s003480050122 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY GBV_ILN_11 GBV_ILN_21 GBV_ILN_32 GBV_ILN_40 GBV_ILN_62 GBV_ILN_65 GBV_ILN_70 GBV_ILN_170 GBV_ILN_185 GBV_ILN_2006 GBV_ILN_2012 GBV_ILN_2014 GBV_ILN_2016 GBV_ILN_2018 GBV_ILN_2020 GBV_ILN_4046 GBV_ILN_4277 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4700 AR 23 1997 5 11 353-360
allfieldsSound	10.1007/s003480050122 doi (DE-627)OLC2074334176 (DE-He213)s003480050122-p DE-627 ger DE-627 rakwb eng 620 530 VZ 530 VZ Kronauer, R. E. verfasserin aut How to estimate the low wavenumber turbulence frequency spectrum 1997 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer-Verlag Berlin Heidelberg 1997 Abstract An estimate of the low wavenumber component of surface turbulence shear stress as a function of frequency has been obtained through measurements of the correlations of the longitudinal component of turbulence velocity made close to the surface at y+=7. The data were acquired in a fully-developed turbulent pipe flow at a Reynolds number (based on centreline velocity and pipe diameter) of 268000, using two single hot-wire anemometer probes. A novel data analysis procedure has been introduced to establish the accuracy limits of the low wavenumber turbulence energy estimate for frequencies in the similarity regime of wall turbulence and the results are compared with other measurement techniques. Reynolds Number Pipe Flow Pipe Diameter Turbulence Velocity Turbulence Shear Hollis, P. G. aut Bullock, K. J. aut Lai, J. C. S. aut Enthalten in Experiments in fluids Springer-Verlag, 1983 23(1997), 5 vom: Nov., Seite 353-360 (DE-627)130443794 (DE-600)710083-8 (DE-576)015977404 0723-4864 nnns volume:23 year:1997 number:5 month:11 pages:353-360 https://doi.org/10.1007/s003480050122 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY GBV_ILN_11 GBV_ILN_21 GBV_ILN_32 GBV_ILN_40 GBV_ILN_62 GBV_ILN_65 GBV_ILN_70 GBV_ILN_170 GBV_ILN_185 GBV_ILN_2006 GBV_ILN_2012 GBV_ILN_2014 GBV_ILN_2016 GBV_ILN_2018 GBV_ILN_2020 GBV_ILN_4046 GBV_ILN_4277 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4700 AR 23 1997 5 11 353-360
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title_sort	how to estimate the low wavenumber turbulence frequency spectrum
title_auth	How to estimate the low wavenumber turbulence frequency spectrum
abstract	Abstract An estimate of the low wavenumber component of surface turbulence shear stress as a function of frequency has been obtained through measurements of the correlations of the longitudinal component of turbulence velocity made close to the surface at y+=7. The data were acquired in a fully-developed turbulent pipe flow at a Reynolds number (based on centreline velocity and pipe diameter) of 268000, using two single hot-wire anemometer probes. A novel data analysis procedure has been introduced to establish the accuracy limits of the low wavenumber turbulence energy estimate for frequencies in the similarity regime of wall turbulence and the results are compared with other measurement techniques. © Springer-Verlag Berlin Heidelberg 1997
abstractGer	Abstract An estimate of the low wavenumber component of surface turbulence shear stress as a function of frequency has been obtained through measurements of the correlations of the longitudinal component of turbulence velocity made close to the surface at y+=7. The data were acquired in a fully-developed turbulent pipe flow at a Reynolds number (based on centreline velocity and pipe diameter) of 268000, using two single hot-wire anemometer probes. A novel data analysis procedure has been introduced to establish the accuracy limits of the low wavenumber turbulence energy estimate for frequencies in the similarity regime of wall turbulence and the results are compared with other measurement techniques. © Springer-Verlag Berlin Heidelberg 1997
abstract_unstemmed	Abstract An estimate of the low wavenumber component of surface turbulence shear stress as a function of frequency has been obtained through measurements of the correlations of the longitudinal component of turbulence velocity made close to the surface at y+=7. The data were acquired in a fully-developed turbulent pipe flow at a Reynolds number (based on centreline velocity and pipe diameter) of 268000, using two single hot-wire anemometer probes. A novel data analysis procedure has been introduced to establish the accuracy limits of the low wavenumber turbulence energy estimate for frequencies in the similarity regime of wall turbulence and the results are compared with other measurement techniques. © Springer-Verlag Berlin Heidelberg 1997
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title_short	How to estimate the low wavenumber turbulence frequency spectrum
url	https://doi.org/10.1007/s003480050122
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author2	Hollis, P. G. Bullock, K. J. Lai, J. C. S.
author2Str	Hollis, P. G. Bullock, K. J. Lai, J. C. S.
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doi_str	10.1007/s003480050122
up_date	2024-07-03T21:54:11.988Z
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