1970
DOI: 10.1115/1.3408482
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Settling Length for Turbulent Flow of Air in Smooth Annuli With Square-Edged or Bellmouth Entrances

Abstract: Settling or hydrodynamic entrance lengths have been determined for turbulent flow of air in three smooth concentric annuli of diameter ratios 0.306, 0.527, and 0.842. Both square-edged and bellmouth entrances were investigated for Reynolds number ranging from 7000–47,500. Flow separation caused by the abrupt change in area of the square-edged entrance resulted in skewed (distorted) velocity profiles near the entrance. This skewness was modified further downstream and finally fully developed velocity profiles w… Show more

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Cited by 1 publication
(3 citation statements)
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“…17 shows that the local turbulent intensity distribution reached its limiting value at the values of (x/De) somewhere between those based on (Umax)x/(U~ax) ~--t.00 and (/x//d) = 1.00. The agreement between the present results and those of Sm~II)HA]~ et al [11] based on (U~a~)~/(Uma~) = 1.00 is good. In this paper, the results in a circular pipe have not been compared with those of the present study as the wall boundary conditions are different.…”
Section: Hydrodynamic Entrance Lengthsupporting
confidence: 88%
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“…17 shows that the local turbulent intensity distribution reached its limiting value at the values of (x/De) somewhere between those based on (Umax)x/(U~ax) ~--t.00 and (/x//d) = 1.00. The agreement between the present results and those of Sm~II)HA]~ et al [11] based on (U~a~)~/(Uma~) = 1.00 is good. In this paper, the results in a circular pipe have not been compared with those of the present study as the wall boundary conditions are different.…”
Section: Hydrodynamic Entrance Lengthsupporting
confidence: 88%
“…The flow in this region of a duet or channel is obviously dependent on the shape of the inlet section. The flow in an entrance with a rounded inlet section is not the same as the flow existing in an entrance with a square-edged inlet section, as shown by experiments [9,10,11]. For a rounded entrance, a reasonably uniform velocity exists at the entrance and one can expect that the boundary-layer will progress from laminar to turbulent.…”
Section: Introductionmentioning
confidence: 85%
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