three-dimensional LES (large eddy simulation) of strut flame-holder with cavity at Ma=0.06 and Ma=0.09 was carried out respectively. The simulation results were compared with experiment data. It showed that the flow field structure of three-dimensional LES was similar with that of experiment. Whats more
two quantitative comparisons in the frequency of wake vortex and time-averaged stream-wise velocity on strut rear section were made. And the maximum relative errors were 9.4% and 7.7% respectively
proving that the model of numerical calculation at boundary conditions was correct and believable. Then by analyzing the three-dimensional flow field of strut
a conclusion that the faster velocity means the bigger size and intensity of wake vortex. Besides
the result of three-dimensional LES shows an obvious phenomenon of three-dimensional effect which gets stronger when the velocity gets faster.
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Related Author
Yuhang LI
Baoyuan WU
Yi WANG
Lixin ZHOU
Yunchuan TAN
Huagui ZHONG
Ruili SUN
Haitao SUN
Related Institution
National Key Laboratory of Science and Technology on Liquid Rocket Engines,Xi'an Aerospace Propulsion Institute,China Aerospace Science and Technology Corporation
Academy of Aerospace Propulsion Technology,China Aerospace Science and Technology Corporation
Sichuan Gas Turbine Establishment,Aero Engine Corporation of China
Beijing Aerospace Institute for Metrology and Measurement Technology, China Academy of Launch Vehicle Technology, China Aerospace Science and Technology Corporation
School of Mechanical Engineering, University of Shanghai for Science and Technology