Experimental investigation of aerosol separation in a rising Taylor bubble
Aerosol transport in rising air bubbles finds application in the removal of micro-pollutants from gases. Its theoretical investigation is mostly limited to small air bubbles because they remain spherical. For bubbles larger than a few centimeters, the gas-liquid interface oscillates in an unpredictable way. This affects the flow on both sides of the interface and ultimately the aerosol-to-liquid capture. We presently investigate aerosol separation in rising Taylor bubbles. Such bubbles have a highly reproducible elongated shape, easily extending to 20 cm in length, and are ideal candidates for model validation. Over one hundred separation experiments with an aerosol size ranging from 1 to 5 μ m are presented. This regime, known as inertia-dominated, is of particular scientific interest because the aerosol transport is strongly dependent on the air flow inside the bubble. A simple and semi-analytical formulation reducing all our experimental results is proposed. • Aerosol separation in rising Taylor bubbles is studied experimentally. • Separation efficiency decreases with bubble elongation. • We propose a semi-analytical model for inertia-dominated aerosol separation. • The model reliably captures the effect of bubble elongation on efficiency.
Authors
- Lars Büttner (ORCID: https://orcid.org/0000-0002-0114-9582)
- Clemens Bilsing (ORCID: https://orcid.org/0000-0002-8577-1546)
- Grégory Lecrivain (ORCID: https://orcid.org/0000-0003-0540-3426)
- Rhandrey Maestri (ORCID: https://orcid.org/0009-0005-6633-0656)
- Uwe Hampel (ORCID: https://orcid.org/0000-0002-7371-0148)
- Jürgen Czarske (ORCID: https://orcid.org/0000-0001-7280-0523)
Institutions
- Helmholtz-Zentrum Dresden-Rossendorf (DE)
- Technische Universität Dresden (DE)
Publication Details
- Journal
- Journal of Aerosol Science
- Published
- 2025-09-10
- DOI
- https://doi.org/10.1016/j.jaerosci.2025.106675
- Primary Topic
- Particle Dynamics in Fluid Flows
- Type
- article
- Field-Weighted Citation Impact
- 0.00