Direct Numerical Simulation of Interaction between Transient Flow and Blade Structure in a Modern Low-Pressure Turbine

نویسندگان

چکیده

• The interaction between the transient flow and blade structure vibration in a modern low-pressure turbine is analysed using high-fidelity direct numerical simulation method. unsteady downstream wakes are highly influenced by vibration. vortex structures directly associated with Unsteady Reynolds Averaged Navier–Stokes (URANS) models not able to capture separation behaviour of flow. At least 5 harmonics required resolve necessary harmonic balance A feature aeronautical Low-Pressure Turbine (LPT) high loadings complex, separated regimes. Most existing research have focused only on analysing such turbines. aerodynamics LPT, however, can be significantly field motion complex non-linear fashion which could lead aeroelastic instabilities as flutter. Therefore, understanding mechanism unsteadiness LPT essential examine stress levels ensure mechanical integrity. novelty this paper, first foremost, method explore flutter forced response T106A turbine, study effects various sources blade. Secondly, paper investigates identifies adequate working ranges method, has been widely used for aeromechanical analysis turbomachines, predicting due fluid-structure an LPT. Another emphasis determination capability model aeroelasticity involving This will bridge key gap knowledge modelling LPTs.

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ژورنال

عنوان ژورنال: International Journal of Mechanical Sciences

سال: 2021

ISSN: ['1879-2162', '0020-7403']

DOI: https://doi.org/10.1016/j.ijmecsci.2020.106104