In order to obtain the three-dimensional flow field of afterburner lobed mixer
a five-hole probe with thermocouple was applied to measure the flow field of the lobed mixer. The velocity and temperature fields in different sections at the lobed mixers outlet were obtained in the experiments
and the change rules of the thermal mixing efficiency and the total pressure recovery coefficient in the flow direction were measured. The experimental results indicate that a pair of inverse direction streamwise vortexes are generated in the trailing edge of lobed mixer
which strengthens the degree of the mixed convection between inner bypass and external bypass. The closer to the trailing edge of the lobed mixer
the greater the mixing degree of the flow between inner bypass and external bypass
the quicker the thermal mixing efficiency increasing
the faster the total pressure recovery coefficient declining.
Effect of lobe number on aerothermodynamic performance of lobed S-shaped two-dimensional nozzle
Mixing characteristics of hyperburner with a lobed mixer
Effect of inlet preswirl on the aerothermodynamic performance of splitter mixing exhaust system
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
Related Author
DU Li-wei
LIU You-hong
SHAO Wan-ren
XU Su
DENG Hong-wei
CHENG Xiao-jun
FAN Yu-xin
CAI Di
Related Institution
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 Engine Design and Research Institute, Aviation Industry Corporation of China
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics
The State Key Laboratory of Mechanical Transmissions, Chongqing University
College of Automotive Engineering, Chongqing University