Enhanced cooling effectiveness in full-coverage film cooling system with impingement jets

Sang Hyun Oh, Dong Hyun Lee, Kyung Min Kim, Moon Young Kim, Hyung Hee Cho

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

11 Citations (Scopus)

Abstract

An experimental investigation is conducted on the cooling effectiveness of full-coverage film cooled wall with impingement jets. Film cooling plate is made of stainless steel, thus the adiabatic film cooling effectiveness and the cooling effect of impingement jet underneath the film cooling plate are comprised in the cooling effectiveness. Infra-red camera is used to measure the temperature of film cooled surfaces. Experiments are conducted with different film cooling hole angles, such as 35° and 90°. Diameters of both film cooling holes and impinging jet holes are 5 mm. The jet Reynolds number base on the hole diameter (Red) ranges from 3,000 to 5,000 and equivalent blowing ratios (M) varies from 0.3 to 0.5, respectively. The distance between the injection plate and the film cooling plate is 1, 3 and 5 times of the hole diameter. The streamwise and spanwise hole spacing to the hole diameter ratio (p/d) are 3 for both the film cooling hole plate and the impingement jet hole plate. The 35° angled film cooling hole arrangement shows higher film cooling effectiveness than the 90° film cooling hole arrangement. As the blowing ratio increases, the cooling effectiveness is enhanced for both the 35° and 90° film cooling hole configurations. For the normal film cooling hole, the film cooling effectiveness is almost constant regardless of H/d, while H/d =1 shows a minimum value for the angled film cooling hole.

Original languageEnglish
Title of host publication2008 Proceedings of the ASME Turbo Expo
Subtitle of host publicationPower for Land, Sea, and Air
Pages735-744
Number of pages10
EditionPART A
DOIs
Publication statusPublished - 2008 Dec 1
Event2008 ASME Turbo Expo - 2008 ASME Turbo Expo, Germany
Duration: 2008 Jun 92008 Jun 13

Publication series

NameProceedings of the ASME Turbo Expo
NumberPART A
Volume4

Other

Other2008 ASME Turbo Expo
CountryGermany
City2008 ASME Turbo Expo
Period08/6/908/6/13

Fingerprint

Cooling systems
Cooling
Blow molding

All Science Journal Classification (ASJC) codes

  • Engineering(all)

Cite this

Oh, S. H., Lee, D. H., Kim, K. M., Kim, M. Y., & Cho, H. H. (2008). Enhanced cooling effectiveness in full-coverage film cooling system with impingement jets. In 2008 Proceedings of the ASME Turbo Expo: Power for Land, Sea, and Air (PART A ed., pp. 735-744). (Proceedings of the ASME Turbo Expo; Vol. 4, No. PART A). https://doi.org/10.1115/GT2008-50784
Oh, Sang Hyun ; Lee, Dong Hyun ; Kim, Kyung Min ; Kim, Moon Young ; Cho, Hyung Hee. / Enhanced cooling effectiveness in full-coverage film cooling system with impingement jets. 2008 Proceedings of the ASME Turbo Expo: Power for Land, Sea, and Air. PART A. ed. 2008. pp. 735-744 (Proceedings of the ASME Turbo Expo; PART A).
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abstract = "An experimental investigation is conducted on the cooling effectiveness of full-coverage film cooled wall with impingement jets. Film cooling plate is made of stainless steel, thus the adiabatic film cooling effectiveness and the cooling effect of impingement jet underneath the film cooling plate are comprised in the cooling effectiveness. Infra-red camera is used to measure the temperature of film cooled surfaces. Experiments are conducted with different film cooling hole angles, such as 35° and 90°. Diameters of both film cooling holes and impinging jet holes are 5 mm. The jet Reynolds number base on the hole diameter (Red) ranges from 3,000 to 5,000 and equivalent blowing ratios (M) varies from 0.3 to 0.5, respectively. The distance between the injection plate and the film cooling plate is 1, 3 and 5 times of the hole diameter. The streamwise and spanwise hole spacing to the hole diameter ratio (p/d) are 3 for both the film cooling hole plate and the impingement jet hole plate. The 35° angled film cooling hole arrangement shows higher film cooling effectiveness than the 90° film cooling hole arrangement. As the blowing ratio increases, the cooling effectiveness is enhanced for both the 35° and 90° film cooling hole configurations. For the normal film cooling hole, the film cooling effectiveness is almost constant regardless of H/d, while H/d =1 shows a minimum value for the angled film cooling hole.",
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Oh, SH, Lee, DH, Kim, KM, Kim, MY & Cho, HH 2008, Enhanced cooling effectiveness in full-coverage film cooling system with impingement jets. in 2008 Proceedings of the ASME Turbo Expo: Power for Land, Sea, and Air. PART A edn, Proceedings of the ASME Turbo Expo, no. PART A, vol. 4, pp. 735-744, 2008 ASME Turbo Expo, 2008 ASME Turbo Expo, Germany, 08/6/9. https://doi.org/10.1115/GT2008-50784

Enhanced cooling effectiveness in full-coverage film cooling system with impingement jets. / Oh, Sang Hyun; Lee, Dong Hyun; Kim, Kyung Min; Kim, Moon Young; Cho, Hyung Hee.

2008 Proceedings of the ASME Turbo Expo: Power for Land, Sea, and Air. PART A. ed. 2008. p. 735-744 (Proceedings of the ASME Turbo Expo; Vol. 4, No. PART A).

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

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Oh SH, Lee DH, Kim KM, Kim MY, Cho HH. Enhanced cooling effectiveness in full-coverage film cooling system with impingement jets. In 2008 Proceedings of the ASME Turbo Expo: Power for Land, Sea, and Air. PART A ed. 2008. p. 735-744. (Proceedings of the ASME Turbo Expo; PART A). https://doi.org/10.1115/GT2008-50784