The present study numerically investigated a conceptual type of internal steam cooling vane with the impingement cooling technology on the basis of plane model and concave model.By changing the inlet Re
distance between the jet and target board and curvature of concave board
a series of temperature value and heat transfer coefficient are obtained.Based on these Results
an impingement cooling vane was designed
which worked on the ANSYSworkbench
and the conjugated heat transfer was studied by means of ANSYS CFX Navier-Stokes code using k-ε two-equation turbulence model for gas field and cooling field.The numerical results of the effects of cooling flow heat transfer in the vane were obtained to evaluate the damage of the vane during steady state operation conditions.
Analysis of matching characteristic of transonic tandem stator airfoil and its optimization
Numerical simulation of a novel turbine inter-vane burner
Comparative numerical simulation of combustion flows in a dual-fuel-combustor
Numerical simulation and design improvement of leading-edge film cooling in an inlet guide vane
Numerical simulation of a steam-cooled vane
Related Author
TAO Yuan
YU Xian-jun
LIU Bao-jie
LI Ming
TANG Hao
ZHANG Chao
CHENG Ben-lin
MO Da
Related Institution
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics,School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics
Admiral Makarov National University of Shipbuilding, Nikolaev
Institute of Engineering Thermophysics, Chinese Academy of Science
Department of Thermal Engineering, Tsinghua University