The design of low-pressure turbines (LPT) must account for the losses generated by the unsteady interaction with the upstream blade row. The estimation of such unsteady wake induced losses requires the accurate prediction of the incoming wake dynamics and decay. Machine-learnt, non-linear turbulence closures (stress-strain relationships) have therefore been developed for LPT flows with unsteady inflow conditions using a zonal based model development approach with an aim to enhance the wake mixing prediction for unsteady Reynolds-averaged Navier-Stokes calculations. Phase-lock averaged data from large eddy simulations at a realistic isentropic exit Reynolds number and two reduced frequencies have been used as a reference in order to create e...
Large eddy simulations were carried out in order to investigate the influence of unsteady incoming w...
AbstractA URANS solver has been applied to the analysis of unsteady effects induced by incoming wake...
Reynolds-Averaged Navier–Stokes (RANS) methods continue to be the backbone of CFD-based design; howe...
Nonlinear turbulence closures were developed that improve the prediction accuracy of wake mixing in ...
This paper presents an assessment of machine-learned turbulence closures, trained for improving wake...
© 2019 Harshal Deepak AkolekarThe design of the gas turbine, which is the work horse of the aviation...
To date no generally accepted prediction method is available for a low pressure turbine designer. De...
Unsteady flow and its effects on the boundary layers of a low pressure turbine blade is complex in n...
Turbines—Part I: Methodology Modern low pressure turbines (LPT) feature high pressure ratios and mod...
This paper presents development of accurate turbulence closures for wake mixing prediction by integr...
Modern low pressure turbines (LPT) feature high pressure ratios and moderate Mach and Reynolds numbe...
In low-pressure turbines (LPT) at design point, around 60–70% of losses are generated in the blade b...
Modern low pressure turbines (LPT) feature high pressure ratios and moderate Mach and Reynolds numbe...
Using a series of direct numerical simulations, the individual and cumulative effects of various dis...
In the present work, direct numerical simulation is employed to investigate the unsteady flow charac...
Large eddy simulations were carried out in order to investigate the influence of unsteady incoming w...
AbstractA URANS solver has been applied to the analysis of unsteady effects induced by incoming wake...
Reynolds-Averaged Navier–Stokes (RANS) methods continue to be the backbone of CFD-based design; howe...
Nonlinear turbulence closures were developed that improve the prediction accuracy of wake mixing in ...
This paper presents an assessment of machine-learned turbulence closures, trained for improving wake...
© 2019 Harshal Deepak AkolekarThe design of the gas turbine, which is the work horse of the aviation...
To date no generally accepted prediction method is available for a low pressure turbine designer. De...
Unsteady flow and its effects on the boundary layers of a low pressure turbine blade is complex in n...
Turbines—Part I: Methodology Modern low pressure turbines (LPT) feature high pressure ratios and mod...
This paper presents development of accurate turbulence closures for wake mixing prediction by integr...
Modern low pressure turbines (LPT) feature high pressure ratios and moderate Mach and Reynolds numbe...
In low-pressure turbines (LPT) at design point, around 60–70% of losses are generated in the blade b...
Modern low pressure turbines (LPT) feature high pressure ratios and moderate Mach and Reynolds numbe...
Using a series of direct numerical simulations, the individual and cumulative effects of various dis...
In the present work, direct numerical simulation is employed to investigate the unsteady flow charac...
Large eddy simulations were carried out in order to investigate the influence of unsteady incoming w...
AbstractA URANS solver has been applied to the analysis of unsteady effects induced by incoming wake...
Reynolds-Averaged Navier–Stokes (RANS) methods continue to be the backbone of CFD-based design; howe...