@misc{10498/39280,
year = {2025},
url = {http://hdl.handle.net/10498/39280},
abstract = {Rotor-stator interactions in turbomachines are characterised by a complex interplay of hydrodynamic instabilities, acoustic pressure waves and receptivity mechanisms, as well as the collision of coherent structures with the blade geometry. An unsteady dual analysis of self-excited instabilities and flow interactions, exemplified by a simple model compressor stage under subsonic conditions, is proposed and presented. Using a low-dissipation sliding-plane implementation, instability-resolving nonlinear-adjoint looping simulations provide detailed sensitivity information that allows for the dissection of the full flow into sub-components linked to distinct flow phenomena. This sensitivity information further links observed flow behaviour to its hydrodynamic or acoustic origin, thereby laying the foundation for a cause-and-effect analysis and for flow control.},
publisher = {Cambridge University Press},
keywords = {computational methods},
keywords = {nonlinear instability},
keywords = {aeroacoustics},
title = {Rotor-stator interactions in a model compressor stage: an unsteady dual analysis},
doi = {10.1017/JFM.2025.10338},
author = {Glazkov, Anton and Fosas de Pando, Miguel Ángel and Schmid, Peter},
}