Due to its great ability to capture almost all the characteristic
properties of turbulent structural flows, the second-order model is successful
in many different interest industries and environment complex problems. These
successes are attributed to the modeling advances of the pressure strain
correlation which controls the strong changes in the turbulence anisotropy. For
this reason, this term is regarded as a modeling Carrefour in this chapter. In
the present work, compressible models involve the turbulent Mach number. the
gradient Mach number and the convective Mach number for this term are examined in
different cases of the compressible homogeneous shear flow and the developed
mixing layers. Comparisons to the universal models and the accepted numerical
data show that the modeling of the pressure strain can be useful for studying
and then understanding the structural compressibility effects.
Author(s) Details
Khlifi
Hechmi
School of Military Aviation, Carthage University, IPEIB, Bizerte,
Naval Academy,Menzel Bourguiba, Bizerte, Laboratory SACES, Borj El Amri 1142,
Tunisia.
Please see the book here:- https://doi.org/10.9734/bpi/strufp/v9/1131
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