This paper presents the comparison of the leading edge separation flow without and with the excitation of select frequency.A variety of excitation effects on the separation flowfield are revealed as(1)delaying separation flow or decreasing separation flow area
(2)modifying turbulence structure
intensifying turbulent activity and enhancing growth rate of separated shear layer
(3)enhancing backflow activity of local region
(4)promoting reattachment and changing separation patterns and vortex distribution
LQ/controller design for aero-engine based on improved NSGAⅡ
Control strategy of active magnetic bearing system based on variable bias current control
APPLICATION OF SQP TO ACCELERATION CONTROL OF TURBOFAN ENGINE
Application of SQP to Multi-Object Optimization of Turbofan Engine Acceleration Control
NUMERICAL SIMULATION OF THREE DIMENSIONAL SHOCK WAVE-BOUNDARY LAYER-SEPERATED FLOW INTERACTIONS
Related Author
WU Qian
HUANG Xiang-hua
LI Qiu-hong
WANG Yuan
ZHOU Hong-kai
WANG Xiao
XU Xin
XIE Zhen-yu
Related Institution
Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics
Department of Design Engineering, Nanjing University of Aeronautics and Astronautics
Jiangsu Key Laboratory of Precision and Micro-Manufacturing Technology, College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics
China National Aero-Technology Import and Export Corporation