Effects of bleed flow on heat/mass transfer in a rotating rib-roughened channel

Yun Heung Jeon, Suk Hwan Park, Kyung Min Kim, Dong Hyun Lee, Hyung Hee Cho

Research output: Chapter in Book/Report/Conference proceedingConference contribution

2 Citations (Scopus)

Abstract

The present study investigates the effects of bleed flow on heat/mass transfer and pressure drop in a rotating channel with transverse rib turbulators. The hydraulic diameter (D h ) of the square channel is 40.0 mm. The bleed holes are located between the rib turburators on the leading surface and the hole diameter (d) is 4.5 mm. The square rib turbulators are installed on both leading and trailing surface. The rib-to-rib pitch (p) is 10.0 times of the rib height (e) and the rib height-to-hydraulic diameter ratio (e/D h ) is 0.055. The tests were conducted at various rotation numbers (0, 0.2, 0.4), while the Reynolds number and the rate of bleed flow to main flow were fixed at 10,000 and 10%, respectively. A naphthalene sublimation method was employed to determine the detailed local heat transfer coefficients using the heat/mass transfer analogy. The results suggest that for a rotating ribbed passage with bleed flow of BR=0.1, the heat/mass transfer on the leading surface is dominantly affected by rib turbulators and the secondary flow induced by rotation rather than bleed flow. The heat/mass transfer on the trailing surface decreases due to the diminution of main flow. The results also show that the friction factor decreases with bleed flow.

Original languageEnglish
Title of host publicationProceedings of the ASME Turbo Expo 2006 - Power for Land, Sea, and Air
Pages877-885
Number of pages9
DOIs
Publication statusPublished - 2006 Nov 15
Event2006 ASME 51st Turbo Expo - Barcelona, Spain
Duration: 2006 May 62006 May 11

Publication series

NameProceedings of the ASME Turbo Expo
Volume3 PART A

Other

Other2006 ASME 51st Turbo Expo
CountrySpain
CityBarcelona
Period06/5/606/5/11

Fingerprint

Mass transfer
Hydraulics
Secondary flow
Sublimation
Naphthalene
Heat transfer coefficients
Pressure drop
Reynolds number
Friction
Hot Temperature

All Science Journal Classification (ASJC) codes

  • Engineering(all)

Cite this

Jeon, Y. H., Park, S. H., Kim, K. M., Lee, D. H., & Cho, H. H. (2006). Effects of bleed flow on heat/mass transfer in a rotating rib-roughened channel. In Proceedings of the ASME Turbo Expo 2006 - Power for Land, Sea, and Air (pp. 877-885). (Proceedings of the ASME Turbo Expo; Vol. 3 PART A). https://doi.org/10.1115/GT2006-91122
Jeon, Yun Heung ; Park, Suk Hwan ; Kim, Kyung Min ; Lee, Dong Hyun ; Cho, Hyung Hee. / Effects of bleed flow on heat/mass transfer in a rotating rib-roughened channel. Proceedings of the ASME Turbo Expo 2006 - Power for Land, Sea, and Air. 2006. pp. 877-885 (Proceedings of the ASME Turbo Expo).
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abstract = "The present study investigates the effects of bleed flow on heat/mass transfer and pressure drop in a rotating channel with transverse rib turbulators. The hydraulic diameter (D h ) of the square channel is 40.0 mm. The bleed holes are located between the rib turburators on the leading surface and the hole diameter (d) is 4.5 mm. The square rib turbulators are installed on both leading and trailing surface. The rib-to-rib pitch (p) is 10.0 times of the rib height (e) and the rib height-to-hydraulic diameter ratio (e/D h ) is 0.055. The tests were conducted at various rotation numbers (0, 0.2, 0.4), while the Reynolds number and the rate of bleed flow to main flow were fixed at 10,000 and 10{\%}, respectively. A naphthalene sublimation method was employed to determine the detailed local heat transfer coefficients using the heat/mass transfer analogy. The results suggest that for a rotating ribbed passage with bleed flow of BR=0.1, the heat/mass transfer on the leading surface is dominantly affected by rib turbulators and the secondary flow induced by rotation rather than bleed flow. The heat/mass transfer on the trailing surface decreases due to the diminution of main flow. The results also show that the friction factor decreases with bleed flow.",
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Jeon, YH, Park, SH, Kim, KM, Lee, DH & Cho, HH 2006, Effects of bleed flow on heat/mass transfer in a rotating rib-roughened channel. in Proceedings of the ASME Turbo Expo 2006 - Power for Land, Sea, and Air. Proceedings of the ASME Turbo Expo, vol. 3 PART A, pp. 877-885, 2006 ASME 51st Turbo Expo, Barcelona, Spain, 06/5/6. https://doi.org/10.1115/GT2006-91122

Effects of bleed flow on heat/mass transfer in a rotating rib-roughened channel. / Jeon, Yun Heung; Park, Suk Hwan; Kim, Kyung Min; Lee, Dong Hyun; Cho, Hyung Hee.

Proceedings of the ASME Turbo Expo 2006 - Power for Land, Sea, and Air. 2006. p. 877-885 (Proceedings of the ASME Turbo Expo; Vol. 3 PART A).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

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N2 - The present study investigates the effects of bleed flow on heat/mass transfer and pressure drop in a rotating channel with transverse rib turbulators. The hydraulic diameter (D h ) of the square channel is 40.0 mm. The bleed holes are located between the rib turburators on the leading surface and the hole diameter (d) is 4.5 mm. The square rib turbulators are installed on both leading and trailing surface. The rib-to-rib pitch (p) is 10.0 times of the rib height (e) and the rib height-to-hydraulic diameter ratio (e/D h ) is 0.055. The tests were conducted at various rotation numbers (0, 0.2, 0.4), while the Reynolds number and the rate of bleed flow to main flow were fixed at 10,000 and 10%, respectively. A naphthalene sublimation method was employed to determine the detailed local heat transfer coefficients using the heat/mass transfer analogy. The results suggest that for a rotating ribbed passage with bleed flow of BR=0.1, the heat/mass transfer on the leading surface is dominantly affected by rib turbulators and the secondary flow induced by rotation rather than bleed flow. The heat/mass transfer on the trailing surface decreases due to the diminution of main flow. The results also show that the friction factor decreases with bleed flow.

AB - The present study investigates the effects of bleed flow on heat/mass transfer and pressure drop in a rotating channel with transverse rib turbulators. The hydraulic diameter (D h ) of the square channel is 40.0 mm. The bleed holes are located between the rib turburators on the leading surface and the hole diameter (d) is 4.5 mm. The square rib turbulators are installed on both leading and trailing surface. The rib-to-rib pitch (p) is 10.0 times of the rib height (e) and the rib height-to-hydraulic diameter ratio (e/D h ) is 0.055. The tests were conducted at various rotation numbers (0, 0.2, 0.4), while the Reynolds number and the rate of bleed flow to main flow were fixed at 10,000 and 10%, respectively. A naphthalene sublimation method was employed to determine the detailed local heat transfer coefficients using the heat/mass transfer analogy. The results suggest that for a rotating ribbed passage with bleed flow of BR=0.1, the heat/mass transfer on the leading surface is dominantly affected by rib turbulators and the secondary flow induced by rotation rather than bleed flow. The heat/mass transfer on the trailing surface decreases due to the diminution of main flow. The results also show that the friction factor decreases with bleed flow.

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M3 - Conference contribution

SN - 079184238X

SN - 9780791842386

T3 - Proceedings of the ASME Turbo Expo

SP - 877

EP - 885

BT - Proceedings of the ASME Turbo Expo 2006 - Power for Land, Sea, and Air

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Jeon YH, Park SH, Kim KM, Lee DH, Cho HH. Effects of bleed flow on heat/mass transfer in a rotating rib-roughened channel. In Proceedings of the ASME Turbo Expo 2006 - Power for Land, Sea, and Air. 2006. p. 877-885. (Proceedings of the ASME Turbo Expo). https://doi.org/10.1115/GT2006-91122