Behaviour of turbulent Prandtl/Schmidt number in compressible mixing layer


Autoria(s): Javed, Afroz; Rajan, NKS; Chakraborty, Debasis
Data(s)

2015

Resumo

The behaviour of turbulent Prandtl/Schmidt number is explored through the model-free simulation results. It has been observed that compressibility affects the Reynolds scalar flux vectors. Reduced peak values are also observed for compressible convective Mach number mixing layer as compared with the incompressible convective Mach number counterpart, indicating a reduction in the mixing of enthalpy and species. Pr-t and Sc-t variations also indicate a reduction in mixing. It is observed that unlike the incompressible case, it is difficult to assign a constant value to these numbers due to their continuous variation in space. Modelling of Pr-t and Sc-t would be necessary to cater for this continuous spatial variation. However, the turbulent Lewis number is evaluated to be near unity for the compressible case, making it necessary to model only one of the Pr-t and Sc-t..

Formato

application/pdf

Identificador

http://eprints.iisc.ernet.in/51692/1/Jou_of_Aero_Eng-229-7-1349-2015.pdf

Javed, Afroz and Rajan, NKS and Chakraborty, Debasis (2015) Behaviour of turbulent Prandtl/Schmidt number in compressible mixing layer. In: PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 229 (7). pp. 1349-1359.

Publicador

SAGE PUBLICATIONS LTD

Relação

http://dx.doi.org/ 10.1177/0954410014547441

http://eprints.iisc.ernet.in/51692/

Palavras-Chave #Aerospace Engineering (Formerly, Aeronautical Engineering)
Tipo

Journal Article

PeerReviewed