INFLUENCE OF AIR COMPRESSIBILITY UPON TIME-AVERAGED QUANTITIES IN FLOW FIELD OF TURBULENT BOUNDARY LAYER
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INFLUENCE OF AIR COMPRESSIBILITY UPON TIME-AVERAGED QUANTITIES IN FLOW FIELD OF TURBULENT BOUNDARY LAYER
Thermal Power GenerationVol. 41, Issue 4, Pages: 30-35(2012)
作者机构:
中国科学院广州能源研究所
作者简介:
基金信息:
DOI:
CLC:TB126
Published:2012
稿件说明:
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ZENG Yuchao, SU Zheng, WU Nengyou, et al. INFLUENCE OF AIR COMPRESSIBILITY UPON TIME-AVERAGED QUANTITIES IN FLOW FIELD OF TURBULENT BOUNDARY LAYER[J]. Thermal power generation, 2012, 41(4): 30-35.
DOI:
ZENG Yuchao, SU Zheng, WU Nengyou, et al. INFLUENCE OF AIR COMPRESSIBILITY UPON TIME-AVERAGED QUANTITIES IN FLOW FIELD OF TURBULENT BOUNDARY LAYER[J]. Thermal power generation, 2012, 41(4): 30-35.DOI:
INFLUENCE OF AIR COMPRESSIBILITY UPON TIME-AVERAGED QUANTITIES IN FLOW FIELD OF TURBULENT BOUNDARY LAYER
In order to study the influence of air compressibility upon the time-averaged quantities in flow field of turbulent boundary layer
a numerical simulation and calculation of 2D flow field in steady turbulent boundary layer with inlet Mach number of 0.058
0.233
0.446
0.872
and 1.457 respectively has been carried out.The results show that the compressibility of air has little influence upon the velocity and temperature distribution in the viscous sublayer zone of the velocity boundary layer and temperature boundary layer
but it can make the velocity and velocity gradient
as well as the temperature and temperature gradient
to be enlarged;the influence of air compressibility upon molecules' diffusion process is utmost small
but has larger influence upon the diffusion process of turbulent flow.When the local Reynolds number is greater than 1×106
and the inlet Mach unmber is larger than 0.466
the local frictional resistance coefficient on the plate will be smaller than that in non-compressible state.Whereas the