Cooling Process of Titanium Alloy Blades After Combustion Using Three Dimensional Heat Flow Coupling Numerical Simulation

Cooling Process of Titanium Alloy Blades After Combustion Using Three Dimensional Heat Flow Coupling Numerical Simulation

In order to understand the cooling procedure of aviation engine blade after titanium combustion, the finite element method was used to simulate the temperature and fluid field of ROTOR37 model after combustion occurred with 550℃ fire proof titanium alloy(TF550 titanium alloy) and 600℃ high temperatu...

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Bibliographic Details
Main Authors: LIANG Xian-ye, MI Guang-bao, LI Pei-jie, CAO Jing-xia, HUANG Xu
Format: Article
Language:zho
Published: Journal of Materials Engineering 2018-10-01
Series:Journal of Materials Engineering
Subjects:
titanium combustion
cooling
three dimensional thermo-fluid couple
numerical simulation
aero-engine
Online Access: http://jme.biam.ac.cn/CN/Y2018/V46/I10/37

Internet

http://jme.biam.ac.cn/CN/Y2018/V46/I10/37

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