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.
2010
01 Pubblicazione su rivista::01a Articolo in rivista
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.
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11573/380849
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