Experiment and Numerical Simulation Investigation of Turbine Blade with Trailing Edge Ejection
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Experiment and Numerical Simulation Investigation of Turbine Blade with Trailing Edge Ejection
Vol. 21, Issue 3, (2006)
作者机构:
西北工业大学 翼型叶栅空气动力学国防重点实验室,陕西,西安,710072
作者简介:
基金信息:
DOI:
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Published:2006
稿件说明:
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WANG Yan-gang, LIU Bo, JIANG Jian, et al. Experiment and Numerical Simulation Investigation of Turbine Blade with Trailing Edge Ejection[J]. 2006, 21(3).
DOI:
WANG Yan-gang, LIU Bo, JIANG Jian, et al. Experiment and Numerical Simulation Investigation of Turbine Blade with Trailing Edge Ejection[J]. 2006, 21(3).DOI:
Experiment and Numerical Simulation Investigation of Turbine Blade with Trailing Edge Ejection
Numerical simulations and tests were carried out to investigate the effect of ejection from different trailing edge slots of a turbine cascade.The detailed flow field of ejection cascade was obtained by using a compact ejection model coupled with the calculation of main flow field.Numerical and experimental results show that the ejection ratio has little effect on the distribution of Mach number and exit flow angle of the two slot types.However
the energy degradation coefficient increases at first and then it has a decreasing tendency with the increase of ejection ratio.The ejection from the symmetric slot blows away the vortex at the blade trailing edge and strengthens the mixing of the wake with the main flow.The ejection from the half slot only blows away the vortex on the slot surface
and has little effect on the flow field near the trailing edge.
Numerical simulation of the three-dimensional flow field of transonic turbine cascade
Upstream wake-passage vortex interaction in turbine cascade
Direct Numerical Flow Simulation in a Two-Dimensional Turbine Cascade
Numerical Investigation of Total-Pressure Recovery Coefficient of Cascade in Unsteady Environment
Adjoint⁃based aerodynamic design optimization of transonic turbine cascades considering different constraints
Related Author
ZENG Jun
XIANG Chuan-guo
CHENG Xin-hua
QI Lei
ZHENG Yun
ZOU Zheng-ping
LIU Huo-xing
LI Wei
Related Institution
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics
Gas Turbine Establishment of China
Aeroengine Numerical Simulation Research Center, National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
China Aviation Powerplant Research Institute
National Key laboratory of Aircraft Engines, Beijing University of Aeronautics and Astronautics