According to the theory of analogy between heat transfer and mass transfer
the mass transfer technique is applied to a shrouded rotor-stator system for experimental
investigation on its heat transfer.An experimental model is set up:The cooling air is blown axially from the front edge of the stator
and the naphthalene(C10H8) sublimation technique is employed to obtain both local and average mass-transfer coefficients for the rotor surface coated by naphthalene.The heat transfer characteristics of the shrouded rotor-stator system are investigated using the mass transfer analog technique.The emphasis is put on analyzing the effects of the following parameters on the transfer characteristics:The ratio of axial gaps Gs 、 the ratio of axial clearance Gc 、the rotational Reynolds number Reθ and flow coefficient Cw .Correlations are obtained experimentally
conclusions are drawn for the test conditions as follows:1.The average mass transfer coefficient increases with increase of the flow coefficient Cw and the rotational Reynolds number Reθ ;2.The average mass transfer coefficient decreases with increase of the ratio of axial gap Gs and the ratio of axial clearance Gc ;3.The peak of local mass transfer coefficient radically moves out with reference to impingement point.
Pressure effect on the heat transfer characteristics of hydrocarbon fuel in the horizontal circular tube at supercritical pressures
Experimental investigation of flow resistance and heat transfer characteristics of typical lamilloy models
AN ENGINEERING EVALUATION SYSTEM OF TURBINE DISC COOLING CONFIGURATION
LOCAL HEAT TRANSFER AND FLOW CHARACTERISTICS OF A ROTATING CAVITY WITH AN AXIAL FRINGE INLET AND A RADIAL OUTLET
AN EXPERIMENTAL STUDY ON LOW CYCLE FATIGUE LIFE OF 1ST TURBINE DISK IN AEROENGINE
Related Author
ZHANG Qi-jun
JIA Zhou-xia
XU Guo-qiang
ZHU Kun
TAO Zhi
WEI Hao-jie
DING Shui-ting
DENG Hong-wu
Related Institution
Academy of Aeronautic Propulsion Technology, Aviation Industry Corporation of China
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics
National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
Gas Turbine Establishment
nd Dept.Nanjing University of Aeronautics and Astronautics