SIMILARITY ANALYSIS AND NUMERICAL SOLUTION OF N-S EQUATIONS FOR LAMINAR FLOW IN A ROTOR-STATOR SYSTEM
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SIMILARITY ANALYSIS AND NUMERICAL SOLUTION OF N-S EQUATIONS FOR LAMINAR FLOW IN A ROTOR-STATOR SYSTEM
Vol. 9, Issue 4, (1994)
作者机构:
1. 西北工业大学
2. 西安石油学院
作者简介:
基金信息:
DOI:
CLC:
Published:1994
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Feng Qing, Zhou Bin, Liu Songling. SIMILARITY ANALYSIS AND NUMERICAL SOLUTION OF N-S EQUATIONS FOR LAMINAR FLOW IN A ROTOR-STATOR SYSTEM[J]. 1994, 9(4).
DOI:
Feng Qing, Zhou Bin, Liu Songling. SIMILARITY ANALYSIS AND NUMERICAL SOLUTION OF N-S EQUATIONS FOR LAMINAR FLOW IN A ROTOR-STATOR SYSTEM[J]. 1994, 9(4).DOI:
SIMILARITY ANALYSIS AND NUMERICAL SOLUTION OF N-S EQUATIONS FOR LAMINAR FLOW IN A ROTOR-STATOR SYSTEM
The similarity analysis for the N S equations and the boundary conditions of a rotor stator system has been completed which shows that the flow field is depedent on five parameters such as inlet flow coefficient
rotational Renolds number
gap ratio
shroud clearance ratio and inlet diameter ratio.The numerical results for the laminar flow field in the system with an axial inflow and a radial outflow have been obtained by the SIMPLE method.It is shown that the gap ratio and the shroud have a great effect on the existence of the rotational core;and the core tends to take form and increase its rotational speed with decreasing the flow coefficient or with increasing the rotational Renolds number.For the closed rotor stator system the results are in good agreement with earlier work done by the other authors.Both the similarity analysis and numerical computation have testified the conclusion that the radial velocity is dominated by inertial terms and the tangential one is dominated by both inertial and viscous terms.The minimum of the flow coefficient required to prevent the ingress of gas into the rotor stator cavity has been calculated
and its linear relation with the rotational Renolds number has been found
which is consistent with the published experimental data very well.
Comparative study on the numerical computation of convective heat transfer over rough surfaces
Numerical simulation of the effect of blade tip blowing on a low speed axial compressor tip clearance flow
Turbulent combustion flow field calculation for afterburner with heat shied
Numerical Method for Calculating the Burst Speed of Axial-Flow-Type Discs
INFLUENCE OF TEMPERATURE RATIO ON PENETRATION DEPTH OF 2D CONFINED CROSS FLOW
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Related Institution
School of Aeronautics Science and Engineering, Beijing University of Aeronautics and Astronautics
Key Laboratory of Condition Monitoring and Control for Power Plant Equipment, Ministry of Education,Department of Power,School of Energy and Power Engineering, North China Electric Power University
College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics
th Dept., Beijing University of Aeronautics and Astronautics