Direct numerical simulation of bubble cavitation at a wall in micro-gravity

Cryogenic tanks used in space applications face challenges due to propellant management, among which is phase change induced by a depressurization. Pool cavitation at the wall in pure methane under micro-gravity conditions is investigated, analyzing its impact on vapor creation and wall heat transfer. A compressible two-phase flow solver, including phase change and conjugate heat transfer, is used. After a validation with available experimental data for single bubble cavitation at the wall in micro-gravity, numerical simulations varying the depressurization amplitude and rate are carried out. Three distinct growth phases are put into evidence: an expansion-controlled phase, occurring within the depressurization time frame, and a transition phase leading to a diffusion-controlled growth where the bubble behaves as in a superheated liquid at constant pressure. Results allow to show the impact that compressible effects have on the phenomenon, and to demonstrate the importance of accounting for a nano-region at the contact line, strongly affecting the wall heat transfer. • A compressible solver with phase change is used to study wall bubble cavitation • The solver is validated with a comparison against experimental data • Results show that the nano-region influences the bubble growth and wall heat transfer • Relative contributions of expansion, variable density and phase change are estimated • The impact of the depressurization amplitude and rate are investigated

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Institutions

Publication Details

Journal
International Journal of Heat and Mass Transfer
Published
2025-08-11
DOI
https://doi.org/10.1016/j.ijheatmasstransfer.2025.127612
Citations
1
Primary Topic
Spacecraft and Cryogenic Technologies
Type
article
Field-Weighted Citation Impact
4.99

Funders

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article

Direct numerical simulation of bubble cavitation at a wall in micro-gravity

Catherine Colin, Sébastien Tanguy, Annafederica Urbano, Maxence Deferrez
1 citations
International Journal of Heat and Mass Transfer
Spacecraft and Cryogenic Technologies
4.99
article

Direct numerical simulation of bubble cavitation at a wall in micro-gravity

Catherine Colin, Sébastien Tanguy, Annafederica Urbano, Maxence Deferrez
article en
1 citations

Abstract

Cryogenic tanks used in space applications face challenges due to propellant management, among which is phase change induced by a depressurization. Pool cavitation at the wall in pure methane under micro-gravity conditions is investigated, analyzing its impact on vapor creation and wall heat transfer. A compressible two-phase flow solver, including phase change and conjugate heat transfer, is used. After a validation with available experimental data for single bubble cavitation at the wall in micro-gravity, numerical simulations varying the depressurization amplitude and rate are carried out. Three distinct growth phases are put into evidence: an expansion-controlled phase, occurring within the depressurization time frame, and a transition phase leading to a diffusion-controlled growth where the bubble behaves as in a superheated liquid at constant pressure. Results allow to show the impact that compressible effects have on the phenomenon, and to demonstrate the importance of accounting for a nano-region at the contact line, strongly affecting the wall heat transfer. • A compressible solver with phase change is used to study wall bubble cavitation • The solver is validated with a comparison against experimental data • Results show that the nano-region influences the bubble growth and wall heat transfer • Relative contributions of expansion, variable density and phase change are estimated • The impact of the depressurization amplitude and rate are investigated

International Journal of Heat and Mass TransferVol. 254
École Nationale de l’Aviation Civile (FR), Centre National de la Recherche Scientifique (FR), Université Fédérale de Toulouse Midi-Pyrénées (FR), Institut Superieur de l'Aeronautique et de l'Espace (ISAE-SUPAERO) (FR), Institut National Polytechnique de Toulouse (FR), Institut de Mécanique des Fluides de Toulouse (FR)
Centre National d’Etudes Spatiales
Climate action
Openalex Percentile: Top 5%
Spacecraft and Cryogenic Technologies
4.99
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