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GeonHwan CHO
GeonHwan CHO
Hanwha Aerospace
在 hanwha.com 的电子邮件经过验证
标题
引用次数
引用次数
年份
Effect of ingress on turbine disks
GH Cho, CM Sangan, J Michael Owen, GD Lock
Journal of Engineering for Gas Turbines and Power 138 (4), 042502, 2016
272016
Use of Pressure Measurements to Determine Effectiveness of Turbine Rim Seals
J Michael Owen, K Wu, JA Scobie, CM Sangan, GH Cho, GD Lock
Journal of Engineering for Gas Turbines and Power 137 (3), 2015
26*2015
Numerical Analysis of Industrial Gas Turbine Secondary Air Systems Employing Vortex Reducers
T Sibilli, GH Cho, F Kholi, A Mucci
ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition, 2018
192018
Solutions of Fourier’s equation appropriate for experiments using thermochromic liquid crystal
O Pountney, GH Cho, GD Lock, JM Owen
International journal of heat and mass transfer 55 (21-22), 5908-5915, 2012
192012
Design optimization of a vane type pre-swirl nozzle
J Lee, H Lee, H Park, GH Cho, D Kim, J Cho
Engineering Applications of Computational Fluid Mechanics 15 (1), 164-179, 2021
172021
Numerical analysis of secondary airflow in a rotating cavity of a gas‐turbine at high operating points with vortex reducer implementation
A Mucci, FK Kholi, T Sibilli, JK Min, MY Ha, GH Cho
Heat and Mass Transfer 57, 1363-1378, 2021
92021
On the measurement and analysis of data from transient heat transfer experiments
GH Cho, H Tang, JM Owen, GD Lock
International Journal of Heat and Mass Transfer 98, 268-276, 2016
82016
Controlling the flow distribution characteristics in the secondary air system of a gas turbine
J Lee, S Kim, D Kim, GH Cho, J Cho
International Journal of Heat and Fluid Flow 95, 108973, 2022
52022
Effect of ingress on flow and heat transfer upstream and downstream of a rotating turbine disc
H Tang, GH Cho, M Patinios, JA Scobie, CM Sangan, JM Owen, GD Lock
Aerospace 6 (5), 49, 2019
42019
Hot gas ingress through turbine rim seals: heat transfer and fluid dynamics
GH Cho
University of Bath, 2014
42014
Turbine apparatus
JW Ha, GH Cho
US Patent 11,162,378, 2021
22021
Swirl Enhancement Effect on Turbine Rim Seal Performance
M Choi, B Goo, GH Cho, SJ Song
Journal of Turbomachinery 146 (5), 2024
12024
반경 간극이 단일 반경 간극 림 씰의 성능에 미치는 영향 측정
구본한, 조건환, 송성진
유체기계 연구개발 발표회 논문집, 179-180, 2019
12019
Turbomachine
SJ Joo, SJ Song, BH Goo, GH Cho
US Patent 11,536,158, 2022
2022
Turbine apparatus
JW Ha, GH Cho
US Patent 11,525,405, 2022
2022
반경방향 분사방식 프리스월 시스템의 프리스월 노즐과 리시버 홀의 상대적 위치에 따른 시스템 성능변화; 반경방향 분사방식 프리스월 시스템의 프리스월 노즐과 리시버 홀의 상대적 위치 …
J Lee, H Lee, G Cho, J Cho
Journal of the Korean Society for Aeronautical & Space Sciences 48 (1), 43-53, 2020
2020
System Performance Variation for Relative Location of Pre-swirl Nozzles and Receiver Holes in Radial On-Board Injection Type Pre-swirl System
J Lee, H Lee, G Cho, J Cho
Journal of the Korean Society for Aeronautical & Space Sciences 48 (1), 43-53, 2020
2020
가스터빈 프리스월 시스템의 유량계수 및 온도강하 효율 향상을 위한 리시버 홀 최적화 전산해석 연구
장세초, 이현규, 조건환, 김동화, 조진수
한국유체기계학회 논문집 22 (6), 45-55, 2019
2019
가스터빈 프리스월 시스템의 외기 온도와 터빈 부하 조건에 따른 탈설계점 특성 분석
박현우, 이정수, 조건환, 조진수
한국항공우주학회지 47 (12), 881-889, 2019
2019
Design of a Single-stage Gas Turbine Research Facility for Ingress Measurement
SJ Choi, M., Goo, B., Kim, H.R., Kim, S., Cho, GH., and Song
International Gas Turbine Congress, 2019
2019
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