A basic relational model for tip leakage mixing loss of unshrouded blades for compressible flow was derived from theoretical analysis of Denton.Relationship.It reflected the influential factors such as blade surface static pressure
chordwise distribution of tip clearance
discharge coefficient and total pressure loss coefficient in the tip region.While only the mixing loss of tip leakage was considered
numerical analysis was performed for the influence of basic load of tip
clearance
average level and chordwise distribution upon mixing loss.The results clearly indicate the governing actions and mechanisms of various factors against the tip leakage mixing loss.Finally
an important combination parameter was put forward to reflect the overall influence of blade loading and tip clearance distribution on the tip leakage mixing loss.
Three-dimension blade optimization of multi-blade fan/compressor
Analysis of flow in a high specific speed mixed flow compressor
Study on aerodynamic optimization design of multistage axial turbine under multiple working conditions
3-D unsteady numerical simulation of fan/compressorwith inlet distortion
Dimension Conversion from Hot State to Cold State of the Turbine Components
Related Author
CHEN Yun-yong
LIU Bo
MA Cong-hui
GAO Li-min
SHI Jian-cheng
WEN Quan
GAO Xing
LIU Bao-jie
Related Institution
National Defence Aerodynamics Laboratory of Airfoil and Cascade, Northwestern Polytechnical University
China Aviation Powerplant Research Institute
National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
School of Energy Science and Engineering, Harbin Institute of Technology
Aeroengine Numerical Simulation Research Center, National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics