Behaviour of turbulent Prandtl/Schmidt number in compressible mixing layer. (June 2015)

• Record Type: Journal Article
• Authors: Javed, Afroz; Rajan, NKS; Chakraborty, Debasis
• Is Part Of: Proceedings of the Institution of Mechanical Engineers. Volume 229:Number 7(2015:Jul.)
• Page Start: 1349
• Page End: 1359
• Publication Date: 2015-06
• Subjects: Compressible mixing layer -- turbulent Prandtl/Schmidt number -- convective Mach number; Aeronautics -- Periodicals; Astronautics -- Periodicals; Airplanes -- Design and construction -- Periodicals; Aerospace industries -- Periodicals; 629.1
• DOI: 10.1177/0954410014547441
• Languages: English
• ISSNs: 0954-4100

Abstract

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. Prt and Sct 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 Prt and Sct 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 Prt and Sct. .