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Heeyoon Chung
Heeyoon Chung
Korea Aerospace Research Institute
Verified email at hanwha.com
Title
Cited by
Cited by
Year
Conjugate heat transfer on full-coverage film cooling with array jet impingements with various Biot numbers
EY Jung, H Chung, SM Choi, T Woo, HH Cho
Experimental Thermal and Fluid Science 83, 1-8, 2017
672017
Augmented heat transfer with intersecting rib in rectangular channels having different aspect ratios
H Chung, JS Park, S Park, SM Choi, DH Rhee, HH Cho
International Journal of Heat and Mass Transfer 88, 357-367, 2015
642015
Thermo-structural analysis of cracks on gas turbine vane segment having multiple airfoils
H Chung, HS Sohn, JS Park, KM Kim, HH Cho
Energy 118, 1275-1285, 2017
392017
Heat transfer measurement near endwall region of first stage gas turbine nozzle having platform misalignment at combustor-turbine interface
H Chung, CW Hong, SH Kim, HH Cho, HK Moon
International Communications in Heat and Mass Transfer 78, 101-111, 2016
372016
Upstream wake effect on flow and heat transfer characteristics at an endwall of first-stage blade of a gas turbine
SM Choi, JS Park, H Chung, S Park, HH Cho
Experimental Thermal and Fluid Science 86, 23-36, 2017
242017
Trailing edge cooling of a gas turbine blade with perforated blockages with inclined holes
H Chung, JS Park, HS Sohn, DH Rhee, HH Cho
International Journal of Heat and Mass Transfer 73, 9-20, 2014
202014
Heat transfer and fluid flow on dimpled surface with bleed flow
H Chung, KM Kim, HG Kwon, S Lee, BS Kim, HH Cho
Heat transfer engineering 35 (6-8), 641-650, 2014
202014
Design of sister hole arrangements to reduce kidney vortex for film cooling enhancement
S Park, H Chung, SM Choi, SH Kim, HH Cho
Journal of Mechanical Science and Technology 31, 3981-3992, 2017
162017
Effect of guide wall on jet impingement cooling in blade leading edge channel
QY Zhao, H Chung, SM Choi, HH Cho
Journal of Mechanical Science and Technology 30, 525-531, 2016
142016
Numerical investigation of the effects of discrete guide vanes on the control of heat transfer on the tip surface of a turbine blade
SM Choi, EY Jung, H Chung, HH Cho
International Journal of Thermal Sciences 112, 142-152, 2017
132017
Effect of shelf squealer tip configuration on aerothermal performance of gas turbine blade
JJ Kim, W Seo, H Chung, M Bang, HH Cho
International Journal of Thermal Sciences 168, 107056, 2021
102021
Optimization of the heating element in a gas-gas heater using an integrated analysis model
YM Lee, H Chung, SH Kim, HS Bae, HH Cho
Energies 10 (12), 1932, 2017
102017
Neural-network-assisted optimization of rectangular channels with intersecting ribs for enhanced thermal performance
A Afzal, H Chung, K Muralidhar, H Hee Cho
Heat Transfer Engineering 41 (18), 1609-1625, 2020
92020
Trailing edge cooling of a gas turbine blade with perforated blockages with inclined holes
H Chung, JS Park, HS Sohn, DH Rhee, HH Cho
Turbo Expo: Power for Land, Sea, and Air 55140, V03AT12A043, 2013
82013
Measurement of Film Cooling Efficiency of Fan-shaped Holes on Endwall of Turbine Blades
H Chung, S Kim, DH Rhee, YS Kang
The KSFM Journal of Fluid Machinery 24 (5), 5-15, 2021
72021
Experimental study on film cooling effectiveness downstream of fan-shaped film cooling holes with staircase geometry at hole exit
S Kim, DE Lee, H Chung, YS Kang, DH Rhee
The KSFM Journal of Fluid Machinery 24 (4), 05-14, 2021
72021
Effect of various rib arrangements on heat transfer in a semicylinder channel with effusion flow
QY Zhao, H Chung, EY Jung, HH Cho
Numerical Heat Transfer, Part A: Applications 71 (5), 547-559, 2017
72017
The effects of hole arrangement and density ratio on the heat transfer coefficient augmentation of fan-shaped film cooling holes
YS Kim, JY Jeong, JS Kwak, H Chung
Energies 14 (1), 186, 2021
62021
Simulation of Aero-propulsion Micro Gas Turbine Engine Using CFD
HY Chung, DH Rhee, YS Kang
2020 KSFM Summer Conference, 2020
62020
Conjugate heat transfer on full-coverage film cooling with array impingement jets
EY Jung, H Chung, SM Choi, T Woo, HH Cho
Turbo Expo: Power for Land, Sea, and Air 56710, V05AT10A025, 2015
62015
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