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사용된 IN738LC 가스 터빈 블레이드 코팅층의 고온 부식 및 Thermally Grown Oxide 형성 거동 최병학, 한성희, 김대현, 안종기, 이재현, 최광수 Korean Journal of Materials Research, 32(4), 200, 2022 |
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Influences of effusion hole diameter on impingement/effusion cooling performance at turbine blade leading edge Zhou JF, Wang XJ, Li J International Journal of Heat and Mass Transfer, 134, 1101, 2019 |
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Modeling and numerical analysis of the effect of blade roughness on particle deposition in a flue gas turbine Xu WW, Zhu KH, Wang JJ, Lin YJ, Li Q Powder Technology, 347, 59, 2019 |
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Effects of blade roughness on particle deposition in flue gas turbines Wang JJ, Lin YJ, Xu WW, Li Q, Dandekar A Powder Technology, 353, 426, 2019 |
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Effects of film cooling hole locations on flow and heat transfer characteristics of impingement/effusion cooling at turbine blade leading edge Zhou JF, Wang XJ, Li J, Li YD International Journal of Heat and Mass Transfer, 126, 192, 2018 |
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Local heat transfer of vortex cooling with multiple tangential nozzles in a gas turbine blade leading edge cooling passage Fan XJ, Li L, Zou JS, Wang JF, Wu F International Journal of Heat and Mass Transfer, 126, 377, 2018 |
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Heat transfer in a rectangular duct with perforated blockages and dimpled side walls Park JS, Jo YH, Kwak JS International Journal of Heat and Mass Transfer, 97, 224, 2016 |
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Air-cooled gas turbine cycles - Part 1: An analytical method for the preliminary assessment of blade cooling flow rates Sciubba E Energy, 83, 104, 2015 |
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Computational analysis of mist/air cooling in a two-pass rectangular rotating channel with 45-deg angled rib turbulators Dhanasekaran TS, Wang T International Journal of Heat and Mass Transfer, 61, 554, 2013 |
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Numerical model validation and prediction of mist/steam cooling in a 180-degree bend tube Dhanasekaran TS, Wang T International Journal of Heat and Mass Transfer, 55(13-14), 3818, 2012 |