Self-similar features of compressible turbulent variable-density mixing layers are studied to provide a validation tool for CFD codes. Self-similar solution is obtained for 2D steady Reynolds averaged Navier-Stokes equations simplified with the boundary layer approximation. Turbulence is treated with eddy viscosity model approach. Two variable turbulent viscosity models are proposed as a refinement of the classical constant turbulent viscosity model: bi-quadratic and Gaussian turbulent viscosity models. Validation of the proposed turbulence models is performed by comparing self-similar solution with experimental data of a helium/air coaxial supersonic jet. Good agreement between the self-similar solution with bi-quadratic turbulent viscosity and experimental data is found. As a consequence, bi-quadratic turbulent viscosity model is selected as turbulence closure for the analytical model. A multi-species CFD code is finally validated by a self-similar solution reproducing a supersonic carbon dioxide axial jet issuing into slow moving air.
Analytical modeling of self-similar compressible turbulent mixing layers / Betti, Barbara; E., Martelli; Nasuti, Francesco. - In: AEROTECNICA MISSILI E SPAZIO. - ISSN 0365-7442. - STAMPA. - 89:(2010), pp. 143-151.
Analytical modeling of self-similar compressible turbulent mixing layers
BETTI, BARBARA;NASUTI, Francesco
2010
Abstract
Self-similar features of compressible turbulent variable-density mixing layers are studied to provide a validation tool for CFD codes. Self-similar solution is obtained for 2D steady Reynolds averaged Navier-Stokes equations simplified with the boundary layer approximation. Turbulence is treated with eddy viscosity model approach. Two variable turbulent viscosity models are proposed as a refinement of the classical constant turbulent viscosity model: bi-quadratic and Gaussian turbulent viscosity models. Validation of the proposed turbulence models is performed by comparing self-similar solution with experimental data of a helium/air coaxial supersonic jet. Good agreement between the self-similar solution with bi-quadratic turbulent viscosity and experimental data is found. As a consequence, bi-quadratic turbulent viscosity model is selected as turbulence closure for the analytical model. A multi-species CFD code is finally validated by a self-similar solution reproducing a supersonic carbon dioxide axial jet issuing into slow moving air.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.