[HTML][HTML] Heat transfer in the trailing region of gas turbines–A state-of-the-art review

W Du, L Luo, Y Jiao, S Wang, X Li, B Sunden - Applied Thermal …, 2021 - Elsevier
Highly efficient gas turbines are beneficial for improving the energy structure, reducing
carbon dioxide emissions and protecting the Earth's environment. A highly efficient gas …

Numerical investigation of heat transfer characteristics of pin-fins with roughed endwalls in gas turbine blade internal cooling channels

KDC Do, DH Chung, DQ Tran, CT Dinh… - International Journal of …, 2022 - Elsevier
In modern jet engines, the effective cooling structure design is essential to both increase
turbine efficiency and, in the meantime, maintain structural integrality. Pin-fin arrays play a …

Film cooling enhancement over oblong-dimpled cutback surfaces for the trailing edge of turbine blades

Y Li, Y Rao, Y Liu, A Terzis - International Journal of Heat and Fluid Flow, 2024 - Elsevier
This study investigates the correspondence between film cooling flow and convective heat
transfer augmentation on the trailing edge cutback surface of a turbine blade, proposing a …

Effects of pin-fins with trapezoidal endwall on heat transfer characteristics in gas turbine blade internal cooling channels

CT Dinh, KDC Do, DH Chung, HS Truong - Journal of Mechanical Science …, 2023 - Springer
All the studies about pin-fins so far focus on investigating the geometry and configurations of
pin-fins to perceive the mechanism of the flow and vortices and maximize the heat transfer …

DES study of the unsteady flow and film cooling at trailing edge cutback with various internal rib configurations

Q Jia, W Du, L Luo, H Yan, X Li, Y Jiao… - Aerospace Science and …, 2024 - Elsevier
Cutback film cooling is widely employed to provide thermal protection for advanced turbine
blade trailing edges (TE). In this study, Detached Eddy Simulation is used to investigate the …

Effects of blowing ratios and lip thicknesses on film cooling for trailing edge cutback with latticework ducts

Q Jia, W Du, X Li, L Luo, Y Jiao, H Yan - Applied Thermal Engineering, 2024 - Elsevier
In this study, a trailing edge cutback configuration with latticework ducts is proposed to
provide more effective thermal protection for high-pressure turbine blades. Detached eddy …

Drag reduction of lift-type Vertical axis wind turbine with slit modified Gurney flap

TP Syawitri, Y Yao, J Yao, B Chandra - Journal of Wind Engineering and …, 2024 - Elsevier
This study examines aerodynamic performance enhancement of Vertical Axis Wind Turbine
(VAWT) blades with Gurney flap (GF) modified by slits. A quasi-3D computational fluid …

Numerical investigation of heat transfer performance and flows characteristics in turbine blade internal cooling using Pin-Fin arrays coupled with discontinuous ribbed …

DL Dao, DA Le, TH Tran, SG Park, GD Pham… - International Journal of …, 2024 - Elsevier
In the scientific domain of cooling techniques research utilizing pin-fins, a number of studies
have concentrated on the configurations of pin-fins. However, recent investigations have …

Effect of the multiple rows of pin-fins on the cooling performance of cutback trailing-edge

L Ye, C Liu, F Zhang, J Li, T Zhou - International Journal of Heat and Mass …, 2021 - Elsevier
Based on heat transfer analyses of trailing-edge cutback configuration, a novel turbulated
cutback structure comprising a combination of pin-fins and cutback surface is proposed in …

Entropy generation rate and proper orthogonal decomposition analysis for unsteady flow and losses of turbine vane cutback

W Du, Q Jia, L Luo, H Yan, S Wang, Y Jiao - Applied Thermal Engineering, 2024 - Elsevier
Trailing edge pressure-side cutback film cooling is a crucial technique to enhance the
thermal protection of advanced turbine vanes. However, unsteady cutback film cooling …