Experimental and numerical investigations for turbine aerodynamic performance with different pressure side squealers and incidence angles

Author:

Chen YingjieORCID,Cai Le,Jiang Dengyu,Li Yiyi,Du Zhengshuai,Wang Songtao

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference46 articles.

1. Loss mechanisms in turbomachines;Denton,1993

2. Averaged and time-dependent aerodynamics of a high pressure turbine blade tip cavity and stationary shroud: Comparison of computational and experimental results;Green,2005

3. Influences of a multi-cavity tip on the blade tip and the over tip casing aerothermal performance in a high pressure turbine cascade;Du;Appl. Therm. Eng.,2019

4. Effect of cavity depth on thermal performance of a cooled blade tip under rotation;Sakaoglu;Int. J. Heat Mass Transf.,2019

5. Measurement of blade tip heat transfer and leakage flow in a turbine cascade with a multi-cavity squealer tip;Park,2013

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