The principal effects of different elliptical and compositive cut at trailing edge of a practical lobed mixer on the thermal mixing efficiency and total-pressure recovery coefficient were studied by three dimensional-computational fluid dynamics(3D-CFD) numerical simulation.The results show that the thermal mixing efficiency declines while the total-pressure recovery coefficient increases as the cut size of the elliptical sector augments.As for the models of compositive cut at trailing edge
the thermal mixing efficiency is lower than that of the original models except for the model with half sector arrangement
but the total-pressure recovery coefficient is usually higher than that of the original model.Among all the models with compositive modification
the model with half sector arrangement has the best performance.
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Related Author
LI Teng
LIU Yong-hong
XIE Yi
WU Fei
SHAO Wan-ren
许羚
卲万仁
谢翌
Related Institution
Shenyang Engine Design and Research Institute, 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
Shenyang Aeroengine Research Institute, Aviation Industry Corporation of China
Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics