Film cooling characteristics of trench film hole fed by the internal cross-flow

Author:

Deng Hefang1ORCID,Teng Jinfang1ORCID,Zhu Mingmin1,Qiang Xiaoqing1,Lu Shaopeng1

Affiliation:

1. School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai¸ P.R. China

Abstract

The paper describes the film cooling characteristics of the trench film hole fed by the internal cross-flow. Three internal cross-flow cases are investigated by using numerical simulations. Results show that the main flow structures of the smooth and 45° rib cases feature helical and asymmetrical, and that of the 135° rib case is straight and symmetrical. When M = 0.5, the film cooling effectiveness η of the 135° rib case is the highest at two cross-flow Reynolds numbers. As [Formula: see text] increases to 1.0, the η of the 135° rib case at Rec = 100,000 is the highest. When [Formula: see text] = 2.0, interestingly, the highest η is achieved by the 45° rib case at Rec = 100,000. The discharge coefficient and total pressure loss coefficient increase with M for the three cases. The discharge coefficient of the 135° rib case is the highest, whereas that of the 45° rib case is the lowest. And the discharge coefficient at Rec = 100,000 is lower than that at Rec = 50,000 because the blockage is more serious at Rec = 100,000, while the total pressure loss coefficient at Rec = 100,000 is higher than that at Rec = 50,000. When Rec = 50,000, the 135° rib case exhibits a higher heat transfer coefficient HTC than the smooth case, while the area-averaged HTC of the 45° rib case depends on the M. When Rec = 100,000, the area-averaged HTC of the 45° rib case is always highest while that of the 135° rib case is always lowest. In addition, the net heat flux reduction ( NHFR) is mainly affected by the η and is more sensitive to the cross-flow at high Rec and low M.

Funder

Innovation Fund from Engineering Research Center of Aerospace Science and Technology, Ministry of Education

the National Science and Technology Main Project

the United Innovation Center (UIC) of Aerothermal Technologies for Turbomachinery

Publisher

SAGE Publications

Subject

Mechanical Engineering,Energy Engineering and Power Technology

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