a Direct Numerical Simulation (DNS) of vortex shedding in a two-dimensional VKI turbine cascade has been carried out.The Reynolds number is 10 000
and the angles of attack are 0 deg
8 deg and -8 deg.The mechanism of unsteady flow in turbine cascade was investigated.Numerical results indicate that
near cascade trailing edge region
clockwise and anticlockwise primary vortices generate alternately from the surface.Secondary vortices form at the interactions of primary vortices and main flow.When secondary vortices mix with the main flow
primary vortices are divided and shedded from trailing edge.The changes of incidence in a certain range have no prominent influences on the development of blade boundary layer.The statistical characteristics and velocity defect characteristics in the wake region are also analyzed.
Numerical simulation of the three-dimensional flow field of transonic turbine cascade
Upstream wake-passage vortex interaction in turbine cascade
Study of phase-lag algorithm for unsteady flow of compressor
Study of performance and profile pressure distribution of transonic compressor under rotor-stator interaction condition
Application of BVF diagnosis on unsteady rotor/stator matching
Related Author
ZENG Jun
XIANG Chuan-guo
CHENG Xin-hua
QI Lei
ZHENG Yun
ZOU Zheng-ping
LIU Huo-xing
LI Wei
Related Institution
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics
Gas Turbine Establishment of China
Aeroengine Numerical Simulation Research Center, National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
China Aviation Powerplant Research Institute
National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics