The convection and heat transfer within the effusion holes of impingement/effusion double wall were optimized to get the maximum internal cooling effect.The ratio of the number of impingement holes to the number of effusion holes per unit area is 1∶3
and the angel of effusion hole is 30 degree.As a hybrid restriction optimization approach
the sequential unconstrained minimization technique was applied for optimization.The optimal results of impingement/effusion double wall were obtained under the pressure drop and unit-area cooling air flow.The results indicate an optimal distribution between the impingement heat transfer and the convective heat transfer within the effusion holes
providing a basis for design of the impingement/effusion double wall for engineering applications.
Model reduction method based on optimization shaping for aero-engine controller
Experiment of cooling effectiveness with double-outlet film hole
Numerical simulation of cooling effectiveness with injection of double-outlet hole
Experimental study of cooling effectiveness of impingement/cocurrent convection/film cooling
Online optimization control of turboshaft engines based on variable inlet guide vane
Related Author
LI Qiu-hong
SUN Jian-guo
XU Guang-hua
LI Guang-chao
LING Xu
KOU Zhi-hai
WU Chao-lin
ZHANG Wei
Related Institution
College of Energy & Power Engineering, Nanjing University of Aeronautics and Astronautics
Liaoning Key Laboratory of Advanced Test Technology for Aeronautical Propulsion System, Faculty of Aerospace Engineering, Shenyang Aerospace University
School of Aerodynamics and Energy Engineering,Shenyang Institute of Aeronautical Engineering
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics
China Aviation Powerplant Research Institute, Aviation Industry Corporation of China