Uncertainty quantification of geometric variations in transonic high-pressure turbine with different trailing edge and throat area distribution

Author:

Chen Yongchao,Zou ZhengpingORCID,Yao Lichao,Wang Yifan

Funder

National Major Science and Technology Projects of China

Publisher

Elsevier BV

Reference51 articles.

1. Axial turbine aerodynamics for aero-engines: flow analysis and aerodynamics design[M];Zou,2018

2. Halila E.E., Lenahan D.T., Thomas TT. Energy efficient engine high pressure turbine test hardware detailed design report[R]. NASA CR-167955, 1982.

3. The trailing edge loss of transonic turbine blades[J];Denton;J. Turbomach.,1990

4. An Examination of the contributions to loss on a transonic turbine blade in cascade[J];Mee;J. Turbomach.,1990

5. Loss mechanisms in turbomachines[J];Denton;J. Turbomach.,1993

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