|
|
|
|
|
Rongdi Zhang, Pengchao Liu, Xirui Zhang, Wenxiong Xi and Jian Liu
With an increased inlet gas temperature and the homogenization of the combustion chamber outlet temperature, the endwalls of gas turbines are exposed to extremely high heat loads. The complex flow structure of turbine endwalls makes it difficult to cool ...
ver más
|
|
|
|
|
|
|
|
|
|
|
Jian Liu, Mengyao Xu and Wenxiong Xi
To protect turbine endwall from heat damage of hot exhaust gas, film cooling is the most significant method. The complex vortex structures on the endwall, such as the development of horseshoe vortices and transverse flow, affects cooling coverage on the ...
ver más
|
|
|
|
|
|
|
|
|
|
|
Holger Werschnik, Marius Schneider, Janina Herrmann, Dimitri Ivanov, Heinz-Peter Schiffer and Christoph Lyko
The aerothermal interaction of the combustor exit flow on the first vane row has been examined at the Large Scale Turbine Rig (LSTR) at Technische Universität Darmstadt (Darmstadt, Germany). A baseline configuration of axial inflow and a variation of swi...
ver más
|
|
|
|
|
|
|
|
|
|
|
Stephen P. Lynch, Karen A. Thole, Atul Kohli, and Christopher Lehane
|
|
|
|
|
|
|
|
|
|
|
Giovanna Barigozzi, Giuseppe Franchini, Antonio Perdichizzi and Marco Quattrore
|
|
|
|
|
|
|
|
|
|
|
N. Sundaram, M. D. Barringer, and K. A. Thole
|
|
|
|
|
|
|
|
|
|
|
N. Sundaram and K. A. Thole
|
|
|
|
|
|
|
|
|
|
|
W. Colban, K. A. Thole, and M. Haendler
|
|
|
|
|
|
|
|
|
|
|
N. Sundaram and K. A. Thole
Pág. 599 - 607
|
|
|
|
|
|
|
|
|
|
|
N. D. Cardwell, N. Sundaram, and K. A. Thole
Pág. 62 - 70
|
|
|
|
|
|