The main destination was to develop the analytical model of rectangular tooth straight through labyrinth seal based on fluid network method.Plenty of computational fluid dynamics simulation data was integrated
and the model was verified by commercial software Flowmaster GT version.The results show that the analytical model developed has high precision
and can be used under complicated conditions including super-sonic flow.Only geometric features and boundary conditions are required for modeling
convergence performs well
and straight through seals with different shapes can be modeled as well.Thus
it can be used as a standard model in secondary air system simulation widely.
Rotating long orifices with radiused inlets analytical model
Effect of gas compressibility on flow coefficient
Algorithm of “turning square into circle” for valve hole
Accurate prediction method of flow coefficient for 2D curved surface variable inlet
Numerical analysis for aeroelastic stability of labyrinth seals
Related Author
TAO Zhi
WU Hong
LI Peng
SHAO Zhiqiang
HU Wencheng
SHEN Chen
WANG Dongdong
DOU Yitao
Related Institution
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics,School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
School of Power and Energy,Northwestern Polytechnical University
Shenyang Engine Research Institute,Aero Engine Corporation of China,Shengyang