The flow field in low pressure turbine guide vane was simulated by third order accuracy Godunov scheme with TVD property.The turbulence model was the combination of B-L algebraic model and MML model.A feature of this guide vane was existence of a long inlet duct with big meridional divergent angle in order to fulfill the requirements of the structure.The numerical simulation and analysis of the vortex structure in flow field indicated that a large separated zone resulted from the divergence of meridional profile.The separated zone not only increased loss before the stator but also increased the size and strength of horseshoe vortex and passage vortex.
High order direct numerical simulation of compressor cascade ,channel separated flow
Multiscale model for incompressible turbulent flows
Effects of vortex generator application on the wing-body juncture horseshoe vortex
EXPERIMENTAL INVESTIGATION ON PERFORMANCE OF A LARGE S-SHAPED DIFFUSER WITH "CARET" INLET
ACOUSTIC CONTROL OF SEPARATED FLOW OVER A 2-DIMENSIONAL AIRFOIL AT DISTURBED INCOMING FLOW
Related Author
LI Yan
ZHU Haitao
BAO Xing-dong
XU Huan
TANG Yang-yang
LI Zhi-qiang
GAO Ge
DONG He
Related Institution
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics
Liaoning Key Laboratory of Digital Techniques Simulation and Test Technology, College of Power and Energy Engineering,Shenyang Aerospace University
The Chinese People's Liberation Army of 94921 Troops,Jinjiang Fujian
School of Power and Energy Engng.Shanghai Jiaotong University