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Auteur principal: Sengupta, Aditi
Format: Preprint
Publié: 2024
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Accès en ligne:https://arxiv.org/abs/2411.12242
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author Sengupta, Aditi
author_facet Sengupta, Aditi
contents The wake-induced transition on the suction surface of a T106A low-pressure turbine (LPT) blade is investigated through a series of implicit large eddy simulations, solving the two-dimensional (2D) compressible Navier-Stokes equations (NSE). The impact of the incoming Gaussian wake amplitude on the blade's profile loss and associated boundary layer parameters is examined, revealing a 50\% reduction in skin friction drag at the highest amplitude. The results indicate that increasing wake amplitude leads to delayed separation and earlier reattachment, resulting in reduced separated flow. The vorticity and enstrophy dynamics during the transition process under varying wake amplitudes reveal characteristic features of wake-induced transition, such as puffs, streaks, and turbulent spots. The periodic passing of wakes induces intermittent "calmed regions", which suppress flow separation and improve profile loss at low Reynolds numbers (Re), typically found in LPTs. The energy budget, accounting for both translational and rotational energy via the turbulent kinetic energy (TKE) and compressible enstrophy transport equation (CETE), respectively, shows trends with increasing wake amplitude. The relative contribution to TKE production and the roles of baroclinicity, compressibility, and viscous terms are explained.
format Preprint
id arxiv_https___arxiv_org_abs_2411_12242
institution arXiv
publishDate 2024
record_format arxiv
spellingShingle Effect of Gaussian wake amplitude on wake-induced transition for a T106A low pressure turbine cascade
Sengupta, Aditi
Fluid Dynamics
The wake-induced transition on the suction surface of a T106A low-pressure turbine (LPT) blade is investigated through a series of implicit large eddy simulations, solving the two-dimensional (2D) compressible Navier-Stokes equations (NSE). The impact of the incoming Gaussian wake amplitude on the blade's profile loss and associated boundary layer parameters is examined, revealing a 50\% reduction in skin friction drag at the highest amplitude. The results indicate that increasing wake amplitude leads to delayed separation and earlier reattachment, resulting in reduced separated flow. The vorticity and enstrophy dynamics during the transition process under varying wake amplitudes reveal characteristic features of wake-induced transition, such as puffs, streaks, and turbulent spots. The periodic passing of wakes induces intermittent "calmed regions", which suppress flow separation and improve profile loss at low Reynolds numbers (Re), typically found in LPTs. The energy budget, accounting for both translational and rotational energy via the turbulent kinetic energy (TKE) and compressible enstrophy transport equation (CETE), respectively, shows trends with increasing wake amplitude. The relative contribution to TKE production and the roles of baroclinicity, compressibility, and viscous terms are explained.
title Effect of Gaussian wake amplitude on wake-induced transition for a T106A low pressure turbine cascade
topic Fluid Dynamics
url https://arxiv.org/abs/2411.12242