The numerical simulation was used to study the effusion holes on the longitudinal wavy liner in the combustor.The investigation focused on the parameters affecting cooling effectiveness
including: opening ratio
height of ripple board
diameter of holes and height of cooling passage.Given the same total flow effusion from holes
the results show that the heat shield gets a higher average cooling effectiveness when the opening ratio is 3% compared with 6%;cooling effectiveness is sensitive to the height of ripple board
the heat shield gets the highest cooling effectiveness when the dimensionless height of ripple board is 1% compared with 2% and 3.33%;but there is a little influence on the cooling effectiveness of the liner with the change of the diameter of holes and the height of cooling passage.
Numerical simulation of film cooling effectiveness with one inlet and double outlet hole on leading edge
Numerical simulation of cooling effectiveness with injection of double-outlet hole
Effect of inaccurate source term loading on simulation ,precision for source term model
Numerical research on film cooling effectiveness with different mainstream pressure gradient
Numerical simulation on film cooling characteristics of heart shaped hole
Related Author
LI Guang-chao
ZHANG Wei
WANG Cheng-jun
PENG Da-wei
WANG Jian-ming
XU Zhi-hui
LI Guang-chao
ZHANG Wei
Related Institution
Liaoning Key Laboratory of Digital Technology Simulation and Test Technique, School of Aero Dynamics and Energy Engineering, Shenyang Aerospace University
School of Aerodynamics and Energy Engineering,Shenyang Institute of Aeronautical Engineering
南京航空航天大学 能源与动力学院 江苏省航空动力系统重点实验室
中国航空发动机集团有限公司 四川燃气涡轮研究院
Aeronautic and Astronautic Engineering College, Air Force Engineering University