TY - JOUR
T1 - Multi-parameter cross-condition scaling of adiabatic film-cooling effectiveness on a turbine vane
AU - Deng, Wei
AU - Ye, Lin
AU - Liang, Xiyuan
AU - Wang, Xinyu
AU - She, Hongxu
AU - Liu, Cunliang
N1 - Publisher Copyright:
© 2026 Published by Elsevier Ltd.
PY - 2026/9
Y1 - 2026/9
N2 - Existing film-cooling scaling studies are mostly based on single-parameter scaling for flat plates and simple hole geometries, which limits their direct applicability to complex vane-passage flows and shaped-hole configurations under gas turbine conditions. Therefore, the present study considers cylindrical holes and 7–7-7 laidback fan-shaped holes at four representative locations on a turbine vane, and employs an experimentally validated CFD approach to investigate the effects of coolant thermophysical properties, momentum ratio (IR), density ratio (DR), and mainstream Reynolds number (Re) on the scaling of adiabatic film-cooling effectiveness. The results show that thermal conductivity and viscosity have minor effects on film-cooling effectiveness, whereas specific heat capacity noticeably affects temperature-based effectiveness (ηt). In contrast, concentration-based effectiveness (ηc) is nearly insensitive to coolant thermophysical properties and serves as a robust similarity metric for scaling engine-condition film-cooling distributions. For flow-parameter matching, IR captures cooling-effectiveness trends and lift-off/reattachment features at low blowing ratio (MR), but its accuracy decreases as MR increases; DR yields the closest agreement with engine-condition ηc distributions, particularly when the coolant film remains attached. Owing to reduced wall-normal momentum and enhanced spanwise spreading, 7–7-7 holes suppress lift-off and show better scaling stability than cylindrical holes. With matched MR and DR, no clear Re self-similar region is identified, and Re mainly affects the intensity of local lift-off/reattachment-related flow-state transitions rather than area-averaged cooling effectiveness. These findings identify the relative roles of coolant properties, hole geometry, and scaling parameters, supporting scaled turbine-vane film-cooling experiments and engine-condition thermal driving-temperature estimation.
AB - Existing film-cooling scaling studies are mostly based on single-parameter scaling for flat plates and simple hole geometries, which limits their direct applicability to complex vane-passage flows and shaped-hole configurations under gas turbine conditions. Therefore, the present study considers cylindrical holes and 7–7-7 laidback fan-shaped holes at four representative locations on a turbine vane, and employs an experimentally validated CFD approach to investigate the effects of coolant thermophysical properties, momentum ratio (IR), density ratio (DR), and mainstream Reynolds number (Re) on the scaling of adiabatic film-cooling effectiveness. The results show that thermal conductivity and viscosity have minor effects on film-cooling effectiveness, whereas specific heat capacity noticeably affects temperature-based effectiveness (ηt). In contrast, concentration-based effectiveness (ηc) is nearly insensitive to coolant thermophysical properties and serves as a robust similarity metric for scaling engine-condition film-cooling distributions. For flow-parameter matching, IR captures cooling-effectiveness trends and lift-off/reattachment features at low blowing ratio (MR), but its accuracy decreases as MR increases; DR yields the closest agreement with engine-condition ηc distributions, particularly when the coolant film remains attached. Owing to reduced wall-normal momentum and enhanced spanwise spreading, 7–7-7 holes suppress lift-off and show better scaling stability than cylindrical holes. With matched MR and DR, no clear Re self-similar region is identified, and Re mainly affects the intensity of local lift-off/reattachment-related flow-state transitions rather than area-averaged cooling effectiveness. These findings identify the relative roles of coolant properties, hole geometry, and scaling parameters, supporting scaled turbine-vane film-cooling experiments and engine-condition thermal driving-temperature estimation.
KW - Concentration-based effectiveness
KW - Density ratio
KW - Film-cooling scaling methodology
KW - Momentum ratio
KW - Reynolds number
KW - Turbine vane
UR - https://www.scopus.com/pages/publications/105043219919
U2 - 10.1016/j.icheatmasstransfer.2026.111902
DO - 10.1016/j.icheatmasstransfer.2026.111902
M3 - 文章
AN - SCOPUS:105043219919
SN - 0735-1933
VL - 178
JO - International Communications in Heat and Mass Transfer
JF - International Communications in Heat and Mass Transfer
IS - P4
M1 - 111902
ER -