Total cooling effectiveness on a staggered full-coverage film cooling plate with impinging jet

Eui Yeop Jung, Dong Hyun Lee, Sang Hyun Oh, Kyung Min Kim, Hyung Hee Cho

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

7 Citations (Scopus)

Abstract

In the present study, total cooling performance was experimentally investigated on a full-coverage film cooling plate with an impingement jet cooling array. The detailed temperature distributions on the film cooled surface were measured using an infra-red thermographic technique. The test plate was made of polycarbonate (k=0.2 W/m•K) and an array jet impinged underneath the test plates. The measured cooling effectiveness is a combined result of film cooling on the surface and convective heat transfer by a jet impingement array underneath the test plate. The diameter (d) of both film cooling and impingement jet cooling holes was 5 mm. Both the streamwise and spanwise hole spacing-to-hole diameter ratios (p/d) were 3 on the film cooled plate and impingement nozzle plate. The inclination angles of the film cooling holes and impingement jet holes were 35° and 90°, respectively. The holes on each plate were arranged in a staggered pattern. The jet Reynolds number based on the hole diameter varied from 3,000 to 7,000 and the equivalent blowing rate (M) changed from 0.3 to 0.7. The combined cooling effectiveness was measured by changing the gap distance between the jet plate and the film cooling plate from 1 to 5 times the hole diameter. The staggered film cooling hole arrangement showed a higher film cooling effectiveness than the inline film cooling hole arrangement. As the blowing rate increased, the cooling effectiveness decreased on the front part of film cooling plate for a fixed height to diameter ratio (H/d). The effect of H/d on the total cooling effectiveness was not significant for the fixed blowing rate (M) in the tested range.

Original languageEnglish
Title of host publicationASME Turbo Expo 2010
Subtitle of host publicationPower for Land, Sea, and Air, GT 2010
Pages1889-1896
Number of pages8
EditionPARTS A AND B
DOIs
Publication statusPublished - 2010 Dec 1
EventASME Turbo Expo 2010: Power for Land, Sea, and Air, GT 2010 - Glasgow, United Kingdom
Duration: 2010 Jun 142010 Jun 18

Publication series

NameProceedings of the ASME Turbo Expo
NumberPARTS A AND B
Volume4

Other

OtherASME Turbo Expo 2010: Power for Land, Sea, and Air, GT 2010
CountryUnited Kingdom
CityGlasgow
Period10/6/1410/6/18

Fingerprint

Cooling
Blow molding
Polycarbonates
Nozzles
Temperature distribution
Reynolds number
Heat transfer
Infrared radiation

All Science Journal Classification (ASJC) codes

  • Engineering(all)

Cite this

Jung, E. Y., Lee, D. H., Oh, S. H., Kim, K. M., & Cho, H. H. (2010). Total cooling effectiveness on a staggered full-coverage film cooling plate with impinging jet. In ASME Turbo Expo 2010: Power for Land, Sea, and Air, GT 2010 (PARTS A AND B ed., pp. 1889-1896). (Proceedings of the ASME Turbo Expo; Vol. 4, No. PARTS A AND B). https://doi.org/10.1115/GT2010-23725
Jung, Eui Yeop ; Lee, Dong Hyun ; Oh, Sang Hyun ; Kim, Kyung Min ; Cho, Hyung Hee. / Total cooling effectiveness on a staggered full-coverage film cooling plate with impinging jet. ASME Turbo Expo 2010: Power for Land, Sea, and Air, GT 2010. PARTS A AND B. ed. 2010. pp. 1889-1896 (Proceedings of the ASME Turbo Expo; PARTS A AND B).
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abstract = "In the present study, total cooling performance was experimentally investigated on a full-coverage film cooling plate with an impingement jet cooling array. The detailed temperature distributions on the film cooled surface were measured using an infra-red thermographic technique. The test plate was made of polycarbonate (k=0.2 W/m•K) and an array jet impinged underneath the test plates. The measured cooling effectiveness is a combined result of film cooling on the surface and convective heat transfer by a jet impingement array underneath the test plate. The diameter (d) of both film cooling and impingement jet cooling holes was 5 mm. Both the streamwise and spanwise hole spacing-to-hole diameter ratios (p/d) were 3 on the film cooled plate and impingement nozzle plate. The inclination angles of the film cooling holes and impingement jet holes were 35° and 90°, respectively. The holes on each plate were arranged in a staggered pattern. The jet Reynolds number based on the hole diameter varied from 3,000 to 7,000 and the equivalent blowing rate (M) changed from 0.3 to 0.7. The combined cooling effectiveness was measured by changing the gap distance between the jet plate and the film cooling plate from 1 to 5 times the hole diameter. The staggered film cooling hole arrangement showed a higher film cooling effectiveness than the inline film cooling hole arrangement. As the blowing rate increased, the cooling effectiveness decreased on the front part of film cooling plate for a fixed height to diameter ratio (H/d). The effect of H/d on the total cooling effectiveness was not significant for the fixed blowing rate (M) in the tested range.",
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Jung, EY, Lee, DH, Oh, SH, Kim, KM & Cho, HH 2010, Total cooling effectiveness on a staggered full-coverage film cooling plate with impinging jet. in ASME Turbo Expo 2010: Power for Land, Sea, and Air, GT 2010. PARTS A AND B edn, Proceedings of the ASME Turbo Expo, no. PARTS A AND B, vol. 4, pp. 1889-1896, ASME Turbo Expo 2010: Power for Land, Sea, and Air, GT 2010, Glasgow, United Kingdom, 10/6/14. https://doi.org/10.1115/GT2010-23725

Total cooling effectiveness on a staggered full-coverage film cooling plate with impinging jet. / Jung, Eui Yeop; Lee, Dong Hyun; Oh, Sang Hyun; Kim, Kyung Min; Cho, Hyung Hee.

ASME Turbo Expo 2010: Power for Land, Sea, and Air, GT 2010. PARTS A AND B. ed. 2010. p. 1889-1896 (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, Lee DH, Oh SH, Kim KM, Cho HH. Total cooling effectiveness on a staggered full-coverage film cooling plate with impinging jet. In ASME Turbo Expo 2010: Power for Land, Sea, and Air, GT 2010. PARTS A AND B ed. 2010. p. 1889-1896. (Proceedings of the ASME Turbo Expo; PARTS A AND B). https://doi.org/10.1115/GT2010-23725