2010
DOI: 10.1016/j.expthermflusci.2009.11.007
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Air flow aerodynamic on a wall-mounted hemisphere for various turbulent boundary layers

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Cited by 45 publications
(18 citation statements)
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“…It is interrelated to the turbulence intensity of the approaching boundary layer. According to previous studies [6,8,23,25] the turbulence level of the oncoming flow influences the length of the recirculation area since with increasing turbulence intensity the location of the separation point is shifted to a further downstream position on the hemisphere. An investigation comparing LES predictions without and with STIG data strongly supports this observation (see Appendix Appendix C).…”
Section: Symmetry Planementioning
confidence: 96%
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“…It is interrelated to the turbulence intensity of the approaching boundary layer. According to previous studies [6,8,23,25] the turbulence level of the oncoming flow influences the length of the recirculation area since with increasing turbulence intensity the location of the separation point is shifted to a further downstream position on the hemisphere. An investigation comparing LES predictions without and with STIG data strongly supports this observation (see Appendix Appendix C).…”
Section: Symmetry Planementioning
confidence: 96%
“…The characteristics of the turbulent flow field were compared with the experimental results mentioned above [14][15][16] strongly focusing on the formation of the separation region on the rear side of the bump. A combined experimental and numerical study was accomplished by Tavakol et al [25]. A hemisphere was immersed in two turbulent boundary layers of different thickness.…”
Section: Introductionmentioning
confidence: 99%
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“…Meroney et al (2002) conducted the numerical simulation to study the mean pressure distribution of an isolated dome and the interference effects between two neighboring domes immersed in a turbulent boundary layer flow. Tavakol et al (2010) experimentally and numerically investigated the flow field around a surface-mounted hemisphere of a fixed height in two different turbulent boundary layers. The results indicated that the RNG k-ε turbulence model overestimates the stream-wise velocity over the hemisphere when the Reynolds number equals to 2.5 Â 10 4 and 3.2 Â 10 4 .…”
Section: Introductionmentioning
confidence: 99%
“…A c c e p t e d M a n u s c r i p t This equation accounts for the beam radiation I beam , diffuse radiation received from the sky I diff 1 and that reflected by the ground I ref which is employed by Eqs. (7) to (9). ρ g is ground reflectance 2 coefficient and is assumed equal to 0.…”
Section: Introductionmentioning
confidence: 99%