Effect of inclined angle on discharge coefficient of the discrete holes in curved wall
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Effect of inclined angle on discharge coefficient of the discrete holes in curved wall
Vol. 22, Issue 7, (2007)
作者机构:
北京航空航天大学能源与动力工程学院 航空发动机气动热力重点实验室,北京,100083
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Published:2007
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ZHANG Chi, ZHAO Meng-meng, LIN Yu-zhen, et al. Effect of inclined angle on discharge coefficient of the discrete holes in curved wall[J]. 2007, 22(7).
DOI:
ZHANG Chi, ZHAO Meng-meng, LIN Yu-zhen, et al. Effect of inclined angle on discharge coefficient of the discrete holes in curved wall[J]. 2007, 22(7).DOI:
Effect of inclined angle on discharge coefficient of the discrete holes in curved wall
An experimental investigation was conducted on the discharge coefficient of multi-holes cooling with different inclined angles in the curved wall for an aircraft engine combustor.The research purpose is to obtain the tendency of the average discharge coefficients with the pressure parameter
one of the most important influencing factors
and to analyze the flow dynamics.The research results indicate that as an aerodynamics factor the pressure parameter has significant impact on the discharge coefficient of the discrete holes for a given geometrical configuration
and for different inclined angles it has different effects.
Influence of rotation on discharge coefficients of two rows of film holes in channel with rib turbulators
A prediction model of film-cooling adiabatic effectiveness based on cohence non-isothermal jet theory
Design and numerical simulation of a transonic swept fan
A new method to control fuel flow of aircraft engine's starting process based on PSO Algorithm
Study of overall cooling effectiveness of discrete holes with different angles to concave wall
Related Author
ZHANG Wei
LI Guang-chao
PENG Da-wei
WANG Cheng-jun
XIANG Song
ZHANG Chi
LIN Yu-zhen
XU Quan-hong
Related Institution
Liaoning Key Laboratory of Digital Technology Simulation and Test Technique,School of Aero Dynamics and Energy Engineering,Shenyang Institute of Aeronautical Engineering
School of Power and Energy,Northwestern Polytechnical University
National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
The key Laboratory of Contemporary Design and Integrated Manufacturing Technology, Ministry of Education, Northwestern Polytechnical University
China Aerospace Science and Technology Corporation