Geometric and numerical simulation models of a forced lobe mixing exhaust system with different lobe numbers were created.Though three-dimensional numerical simulation
the principle of effect of different lobe numbers in a forced mixing exhaust system was obtained.The results show that
non-dimensional average streamwise vorticities increase at the trailing edge of the lobe mixer with the growing number of lobe.At the exit section of the forced mixing exhaust system
thermal mixing efficiency declines as the lobe number increases;and the total-pressure recovery coefficient firstly increases when the lobe number increases from 8 to 16
then declines when it augments from 16 to 20 and finally increases when it rises from 20 to 24.
Effect of ratio of height to width of lobe on performance of forced mixing exhaust system
Effect of elliptical and compositive cut at trailing edge on the performance of a lobed mixer
Effect of lobe number on aerothermodynamic performance of lobed S-shaped two-dimensional nozzle
Mixing characteristics of hyperburner with a lobed mixer
Experiment of flow field in lobed mixer
Related Author
LI Teng
LIU Yong-hong
XIE Yi
SHAO Wan-ren
WU Fei
LIU You-hong
XIE Yi
GUO Nan
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
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics
Shenyang Engine Design and Research Institute, Aviation Industry Corporation of China, Shengyang
Shenyang Aeroengine Design and Research Institute, Aviation Industry Corporation of China