Efficient unsteady simulations of cooled turbines are essential for improving thermal load predictions and optimising turbine design. This study introduces a combined approach of the Harmonic Balance method, a differential Reynolds stress model, and a localised film cooling model, which captures the dominant unsteady effects in high-pressure turbine rotors. Traditional steady-state RANS simulations often under- or over-predict adiabatic wall temperatures and heat transfer coefficients due to the neglect of unsteady interactions. Results show that unsteady effects significantly impact thermal loads, with frequency-domain harmonic balance simulations closely matching high-fidelity time-domain URANS results at a fraction of the computational expense. The localised film cooling model improves accuracy over a coarser volume source model, while the SSG/LRR-log(w) turbulence model enhances turbulent mixing predictions. This can enable a much better capturing of relevant unsteady effects and turbulent mixing processes in both problem analysis and design, the impact of which would remain unknown using simpler methods.
Müller et al. (Mon,) studied this question.
Synapse has enriched 5 closely related papers on similar clinical questions. Consider them for comparative context: