Heat transfer characteristics of an angled array impinging jet on a concave duct

Eui Yeop Jung, Chan Ung Park, Dong Hyun Lee, Kyung Min Kim, Ta Kwan Woo, Hyung Hee Cho

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

3 Citations (Scopus)

Abstract

This study investigated the heat transfer characteristics of an array jet cooling system on a concave surface. Two types of injection holes were used: one for impinging jets normal to the impingement surface, and the other for angled impinging jets. For the normal jets, the jet Reynolds number (Re) based on the hole diameter varied from 3,000 to 10,000, and the heightto- diameter ratio (H/d) was fixed at 1.0. There were 15 injection holes positioned in a staggered 3×5 array. For the angled jets, Re was set to 5,000 and H/d was also fixed at 1.0. Naphthalene sublimation method was used to determine the heat transfer coefficients on the targeted plates. For normal impinging jet cooling, separate peaks were observed at the stagnation regions due to the curvature effect. Since a crossflow was generated by air spent from the jet arrays, the crossflow effect increased as it moved downstream. Due to the interaction between the crossflow and impinging jets, the peak values at the stagnation points increased downstream. The heat transfer coefficient on the targeted plate increased with Re. The average Sh of the angled jets was higher than that of the normal jets, as the obliquely impinging jet increased the mass flow rate and mass interaction between the jet impingement points.

Original languageEnglish
Title of host publicationASME Turbo Expo 2012
Subtitle of host publicationTurbine Technical Conference and Exposition, GT 2012
Pages601-607
Number of pages7
EditionPARTS A AND B
DOIs
Publication statusPublished - 2012 Dec 1
EventASME Turbo Expo 2012: Turbine Technical Conference and Exposition, GT 2012 - Copenhagen, Denmark
Duration: 2012 Jun 112012 Jun 15

Publication series

NameProceedings of the ASME Turbo Expo
NumberPARTS A AND B
Volume4

Other

OtherASME Turbo Expo 2012: Turbine Technical Conference and Exposition, GT 2012
CountryDenmark
CityCopenhagen
Period12/6/1112/6/15

Fingerprint

Ducts
Heat transfer
Heat transfer coefficients
Sublimation
Naphthalene
Cooling systems
Reynolds number
Flow rate
Cooling

All Science Journal Classification (ASJC) codes

  • Engineering(all)

Cite this

Jung, E. Y., Park, C. U., Lee, D. H., Kim, K. M., Woo, T. K., & Cho, H. H. (2012). Heat transfer characteristics of an angled array impinging jet on a concave duct. In ASME Turbo Expo 2012: Turbine Technical Conference and Exposition, GT 2012 (PARTS A AND B ed., pp. 601-607). (Proceedings of the ASME Turbo Expo; Vol. 4, No. PARTS A AND B). https://doi.org/10.1115/GT2012-69566
Jung, Eui Yeop ; Park, Chan Ung ; Lee, Dong Hyun ; Kim, Kyung Min ; Woo, Ta Kwan ; Cho, Hyung Hee. / Heat transfer characteristics of an angled array impinging jet on a concave duct. ASME Turbo Expo 2012: Turbine Technical Conference and Exposition, GT 2012. PARTS A AND B. ed. 2012. pp. 601-607 (Proceedings of the ASME Turbo Expo; PARTS A AND B).
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abstract = "This study investigated the heat transfer characteristics of an array jet cooling system on a concave surface. Two types of injection holes were used: one for impinging jets normal to the impingement surface, and the other for angled impinging jets. For the normal jets, the jet Reynolds number (Re) based on the hole diameter varied from 3,000 to 10,000, and the heightto- diameter ratio (H/d) was fixed at 1.0. There were 15 injection holes positioned in a staggered 3×5 array. For the angled jets, Re was set to 5,000 and H/d was also fixed at 1.0. Naphthalene sublimation method was used to determine the heat transfer coefficients on the targeted plates. For normal impinging jet cooling, separate peaks were observed at the stagnation regions due to the curvature effect. Since a crossflow was generated by air spent from the jet arrays, the crossflow effect increased as it moved downstream. Due to the interaction between the crossflow and impinging jets, the peak values at the stagnation points increased downstream. The heat transfer coefficient on the targeted plate increased with Re. The average Sh of the angled jets was higher than that of the normal jets, as the obliquely impinging jet increased the mass flow rate and mass interaction between the jet impingement points.",
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Jung, EY, Park, CU, Lee, DH, Kim, KM, Woo, TK & Cho, HH 2012, Heat transfer characteristics of an angled array impinging jet on a concave duct. in ASME Turbo Expo 2012: Turbine Technical Conference and Exposition, GT 2012. PARTS A AND B edn, Proceedings of the ASME Turbo Expo, no. PARTS A AND B, vol. 4, pp. 601-607, ASME Turbo Expo 2012: Turbine Technical Conference and Exposition, GT 2012, Copenhagen, Denmark, 12/6/11. https://doi.org/10.1115/GT2012-69566

Heat transfer characteristics of an angled array impinging jet on a concave duct. / Jung, Eui Yeop; Park, Chan Ung; Lee, Dong Hyun; Kim, Kyung Min; Woo, Ta Kwan; Cho, Hyung Hee.

ASME Turbo Expo 2012: Turbine Technical Conference and Exposition, GT 2012. PARTS A AND B. ed. 2012. p. 601-607 (Proceedings of the ASME Turbo Expo; Vol. 4, No. PARTS A AND B).

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

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Jung EY, Park CU, Lee DH, Kim KM, Woo TK, Cho HH. Heat transfer characteristics of an angled array impinging jet on a concave duct. In ASME Turbo Expo 2012: Turbine Technical Conference and Exposition, GT 2012. PARTS A AND B ed. 2012. p. 601-607. (Proceedings of the ASME Turbo Expo; PARTS A AND B). https://doi.org/10.1115/GT2012-69566