Abstract
The present study investigates the pressure drop characteristics of rotating two-pass ducts. The duct has an aspect ratio (W/H) of 0.5 and a hydraulic diameter (D h ) of 26.67 mm. Rib turbulators are attached in the four different cross arrangements on the leading and trailing surfaces of the test ducts. The ribs have a rectangular cross section of 2 mm (e) × 3 mm (w) and a rib angle-of-attack of 70°. The pitch-to-rib-height ratio (p/e) is 7.5 and the rib-height-to-hydraulic-diameter ratio (e/D h ) is 0.075. The measured results for each region show that the highest pressure drop appears in the turning region in the stationary case, but appears in the upstream region of the second pass in the rotating case. The heat transfer and the pressure coefficients in the first pass are similar for the stationary and rotating cases in all the tested rib arrangements. After the turning region, however, the heat transfer and pressure drop are high in the cases with the cross NN- and PP-type ribs in the stationary ducts. In the rotating ducts, they are high in the cases with the cross NP- and PP-type ribs.
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Abbreviations
- C p :
-
non-dimensional pressure drop coefficient, Eq. (1)
- D h :
-
duct hydraulic diameter (m)
- D naph :
-
mass diffusion coefficient of naphthalene vapor in air (m2 s−1)
- e :
-
rib height (m)
- f :
-
friction factor, Eq. (2)
- f 0 :
-
friction factor of a fully developed turbulent flow in a stationary smooth pipe
- h m :
-
mass transfer coefficient (m s−1)
- H :
-
passage height (m)
- p :
-
rib-to-rib pitch
- P ref :
-
reference pressure
- P x :
-
local pressure
- Re :
-
Reynolds number, D h u b /ν
- Ro :
-
Rotation number, D h Ω/u b
- Sh :
-
Sherwood number, h m D h /D naph
- Sh 0 :
-
Sherwood number of a fully developed turbulent flow in a smooth pipe
- \( \overline{{Sh}} \) :
-
regional averaged Sherwood number
- u b :
-
mean flow velocity (m s−1)
- w :
-
width of the rib (m)
- W :
-
width of the passage (m)
- x :
-
streamwise distance from the rotating axis
- y :
-
lateral distance from the center of channel
- z :
-
distance from the center toward vertical direction
- α :
-
rib angle-of-attack
- η :
-
thermal performance, Eq. (3)
- μ :
-
dynamic viscosity
- ν :
-
kinematic viscosity
- ρ :
-
density of the fluid
- Ω :
-
angular velocity
References
Han JC, Park JS (1988) Developing heat transfer in rectangular channels with rib turbulators. Int J Heat Mass Transf 31(1):183–195
Taslim ME, Li T, Kercher DM (1996) Experimental heat transfer and friction in channels roughened with angled, V-shaped, and discrete ribs on two opposite walls. ASME J Turbomachinery 118:20–28
Bohnhoff B, Parneix S, Leusch J, Johnson BV, Schabacker J, Bolcs A (1999) Experimental and numerical study of developed flow and heat transfer in coolant channels with 45 degree ribs. Int J Heat Fluid Flow 20:311–319
Cho HH, Wu SJ, Kwon HJ (2000) Local heat/mass transfer measurements in a rectangular duct with discrete ribs. ASME J Turbomachinery 122:1–8
Astarita T, Cardon G (2000) Thermofluidynamic analysis of the flow in a sharp 180° turn channel. Exp Term Fluid Sci 20:188–200
Liou TM, Tzeng YY, Chen CC (1999) Fluid flow in a 180 deg sharp turning duct with different divider thickness. ASME J Turbomachinery 121:569–576
Metzger DE, Sahm MK (1986) Heat transfer around sharp 180-deg turns in smooth rectangular channels. ASME J Heat Transf 108:500–506
Chyu MK (1991) Regional heat transfer in two-pass and three-pass passages with 180-deg sharp turns. ASME J Heat Transf 113:63–70
Mokizuchi S, Murata A, Shibata R, Yang WJ (1999) Detailed measurements of local heat transfer coefficients in turbulent flow through smooth and rib-roughened serpentine passages with a 180° sharp bend. Int J Heat Mass Transf 42:1925–1934
Iacovides H, Jackson DC, Ji H, Kelemenis G, Launder BE, Nikas K (1998) LDA study of the flow development through an orthogonally rotating U-bend of strong curvature and rib-roughened walls. ASME J Turbomachinery 120:386–391
Azad GS, Uddin HJ, Han JC, Moon HK, Glezer B (2002) Heat transfer in a two-pass rectangular rotating channel with 45° angled rib turbulators. ASME J Turbomachinery 124:251–259
Hwang JJ, Tsai YP, Wang WJ, Lai DY (1999) Effects of leading-wall blowing/suction on mixed convective phenomena in a radially rotating multiple-pass duct. Int J Heat Mass Transf 42:4461–4474
Bons JP, Kerrebrock JL (1999) Complementary velocity and heat transfer measurements in a rotating cooling passage with smooth walls. ASME J Turbomachinery 121:651–662
Wanger JH, Johnson BV, Kopper FC (1991) Heat transfer in rotating serpentine passages with smooth walls. ASME J Turbomachinery 113:321–330
Cho HH, Lee SY, Won JH, Rhee DH (2004) Heat/mass transfer in a two-pass rotating rectangular duct with and without 70°-angled ribs. Heat Mass Transf 40:467–475
Cho HH, Lee SY, Rhee DH (2004) Effects of cross ribs on heat/mass transfer in a two-pass rotating duct. Heat Mass Transf 40:743–755
Kim KM, Kim YY, Lee DH, Rhee DH, Cho HH (2006) Local heat/mass transfer phenomena in rotating passage, Part 2: angled ribbed passage. AIAA J Thermophys Heat Transf 20(2):199–210
Kline SJ, McClintock FA (1953) Describing uncertainty in single-sample experiments. Mech Eng 75:3–8
Petukhov BS (1970) Heat transfer and friction in turbulent pipe flow with various physical properties. Advances in heat transfer 6, Academic, New York, pp 503–564
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This work was supported partially by the Electric Power Industry Technology Evaluation and Planning.
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Kim, K.M., Lee, D.H. & Cho, H.H. Pressure drop and thermal performance in rotating two-pass ducts with various cross rib arrangements. Heat Mass Transfer 44, 913–919 (2008). https://doi.org/10.1007/s00231-007-0331-y
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DOI: https://doi.org/10.1007/s00231-007-0331-y