TY - JOUR
T1 - Prediction of compressible turbulent boundary layer via a symmetry-based length model
AU - She, Zhen Su
AU - Zou, Hong Yue
AU - Xiao, Meng Juan
AU - Chen, Xi
AU - Hussain, Fazle
N1 - Publisher Copyright:
© 2018 Cambridge University Press.
PY - 2018/12/25
Y1 - 2018/12/25
N2 - A recently developed symmetry-based theory is extended to derive an algebraic model for compressible turbulent boundary layers (CTBL)-predicting mean profiles of velocity, temperature and density-valid from incompressible to hypersonic flow regimes, thus achieving a Mach number invariant description. The theory leads to a multi-layer analytic form of a stress length function which yields a closure of the mean momentum equation. A generalized Reynolds analogy is then employed to predict the turbulent heat transfer. The mean profiles and the friction coefficient are compared with direct numerical simulations of CTBL for a range of from 0 (e.g. incompressible) to 6.0 (e.g. hypersonic), with an accuracy notably superior to popular current models such as Baldwin-Lomax and Spalart-Allmaras models. Further analysis shows that the modification is due to an improved eddy viscosity function compared to competing models. The results confirm the validity of our-invariant stress length function and suggest the path for developing turbulent boundary layer models which incorporate the multi-layer structure.
AB - A recently developed symmetry-based theory is extended to derive an algebraic model for compressible turbulent boundary layers (CTBL)-predicting mean profiles of velocity, temperature and density-valid from incompressible to hypersonic flow regimes, thus achieving a Mach number invariant description. The theory leads to a multi-layer analytic form of a stress length function which yields a closure of the mean momentum equation. A generalized Reynolds analogy is then employed to predict the turbulent heat transfer. The mean profiles and the friction coefficient are compared with direct numerical simulations of CTBL for a range of from 0 (e.g. incompressible) to 6.0 (e.g. hypersonic), with an accuracy notably superior to popular current models such as Baldwin-Lomax and Spalart-Allmaras models. Further analysis shows that the modification is due to an improved eddy viscosity function compared to competing models. The results confirm the validity of our-invariant stress length function and suggest the path for developing turbulent boundary layer models which incorporate the multi-layer structure.
KW - compressible boundary layers
KW - compressible turbulence
KW - turbulence modelling
UR - http://www.scopus.com/inward/record.url?scp=85055432584&partnerID=8YFLogxK
U2 - 10.1017/jfm.2018.710
DO - 10.1017/jfm.2018.710
M3 - Article
AN - SCOPUS:85055432584
SN - 0022-1120
VL - 857
SP - 449
EP - 468
JO - Journal of Fluid Mechanics
JF - Journal of Fluid Mechanics
ER -