The principle of effect of different cut angles at trailing edge of a practical lobed mixer on the thermal efficiency and the total-pressure recovery coefficient was studied by 3D-CFD(computational fluid dynamics)numerical simulation.The results show that
when the angles cut at trailing edge of the lobed mixer vary from 2.5° to 15°
the thermal efficiency augments and the total-pressure recovery coefficient decline as the angle increases
and when the cut angles vary from 15° to 60°
the thermal efficiency declines and the total-pressure recovery coefficient augments as the angle increases.
Effect of ratio of height to width of lobe on performance of forced mixing exhaust system
Effect of lobe numbers on the performance of a lobed mixer in the forced mixing exhaust system
Effect of elliptical and compositive cut at trailing edge on the performance of a lobed mixer
Effects of interfacial contact area and streamwise vortices on pumping ratio of lobed mixer
Effect of lobe number on aerothermodynamic performance of lobed S-shaped two-dimensional nozzle
Related Author
LI Teng
LIU Yong-hong
XIE Yi
SHAO Wan-ren
WU Fei
刘友宏
樊超
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
China Helicopter Research and Development Institute, Aviation Industry Corporation of China
Collaborative Innovation Center for Advanced Aero-Engine