期刊： JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2021; 143 (8)
Effective cooling structure design in the trailing edge (TE) of a high pressure turbine (HPT) blade is essential to increase turbine efficiency and ma......
期刊： JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2021; 143 (7)
The three-pass turbulated serpentine channel has many applications in internal turbine blade systems. However, the studies on the effects of the outfl......
期刊： JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2021; 143 (9)
Leading-edge multi-channel double-wall design, a novel internal cooling structure, has been presented recently to enable higher overall cooling effect......
期刊： JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2021; 143 (6)
With the increase of turbine inlet temperature and the application of premixed combustion, turbine components, particularly the turbine endwall, work ......
期刊： JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2021; 143 (6)
Control of corner separation in axial compressor blade rows has attracted much interest due to its potential to improve compressor efficiency and the ......
期刊： JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2021; 143 (6)
To survive in a complex environment, nature has produced efficient and versatile resource-rich structures. One of the novel drag reduction designs com......
期刊： JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2021; 143 (8)
Gas turbines have been widely used. With the continuous improvement of the performance of gas turbines, the turbine inlet temperature has greatly exce......
期刊： JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2021; 143 (4)
Effective coolant schemes are required for providing cooling to the first-stage stator vanes of gas turbines. To correctly predict coolant performance......
期刊： JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2021; 143 (4)
The stators of the first stage of a gas turbine are exposed to severe temperatures. The coolant streams introduced to prevent the stators from thermal......
期刊： JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2021; 143 (10)
An experimental study was conducted to characterize the evolution of turbulent boundary layer flow over a micro-rib-dimple-structured surface. In addi......
期刊： JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2021; 143 (9)
The non-uniform disturbance in the circumferential direction is the essential cause of the occurrence of rotating stall in a turbomachinery. In order ......
期刊： JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2021; 143 (8)
Experimental and numerical methods were used to investigate the aerodynamic effects of a near-casing streamwise incoming vortex flow on the tip leakag......
期刊： JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2021; 143 (6)
A signal reconstruction algorithm based on the compressed sensing (CS) theory with dual-uniform sampling point (DUSP) distribution is developed and ap......
期刊： JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2021; 143 (5)
The inverse design method for turbomachinery can directly acquire a blade geometry with specific aerodynamic parameters, such as pressure loading on t......
期刊： JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2021; 143 (4)
One-dimensional laterally averaged adiabatic film cooling effectiveness (eta) over bar (lat)-based correlations have been widely employed in the cooli......
