A unilateral statistical average scheme is used to derive a new set of closed equations of incompressible turbulent flows
which is capable of describing both of statistical mean flow and intermittent coherent flow without introducing any empirical treatments and coefficients.Besides the special average scheme
the concepts of symmetic drift flows
orthotropic trubulence and the chain of momentum transference are also used in the original derivation.More important
the obtained energy equation of series form suggests that the infinite terms in the equation are corresponding to infinite layers of structures of trubulence.If all the terms of the series are taken for determining the length scale
one obtains statistical mean results.On the other hand
if only parts of terms are taken
coherent flows would appear.To verify the adaptablity of the equations
three benchmark flows
i.e.free shear flow
boundary layer transition flow and separated flow
are numerically simulated on PC computers.Both of accurate results of statistical mean flows and vivid structures of coherent flows are obtained.
Large eddy simulation of supersonic jet mixing flow
Comparison and analysis of WENO schemes base on supersonic boundary layer transition
Numerical investigation of impressible turbulent flows past airfoils
Dispersion model for incompressible turbulent flows
Numerical simulation of the breakdown process in laminar-turbulent transition of incompressible boundary layer on a flat plate
Related Author
潘宏禄
程晓丽
朱志斌
WANG Hong-bo
SUN Ming-bo
WANG Zhen-guo
LIU Chao-yang
TANG Yang-yang
Related Institution
中国航天科技集团有限公司 中国航天空气动力技术研究院
College of Aerospace Science and Engineering, National University of Defense Technology
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics
Science and Technology Division, Civil Aviation University of China