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Synchrotron radiography of wire-driven cylindrically converging shock waves interacting with a cylindrical bubble
KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics. (FLOW)ORCID iD: 0009-0002-7782-7279
KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics. (FLOW)ORCID iD: 0000-0002-2524-4058
KTH, School of Engineering Sciences (SCI), Engineering Mechanics. (FLOW)ORCID iD: 0000-0003-3602-156X
KTH, School of Engineering Sciences (SCI), Engineering Mechanics. (FLOW)ORCID iD: 0000-0002-4236-2793
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2026 (English)In: Journal of Fluid Mechanics, ISSN 0022-1120, E-ISSN 1469-7645, Vol. 1033, article id A29Article in journal (Refereed) Published
Abstract [en]

The interaction between cylindrically converging shock waves (SWs) in a water–gelatine solution and a coaxial cylindrical air bubble is studied experimentally and numerically. Two configurations are considered: (i) an azimuthally symmetric, cylindrically converging SW of Mach 1.35 impinging on a coaxial cylindrical bubble, and (ii) a semicylindrical converging SW of Mach 1.45 (corresponding to half of the cylindrical front), interacting with the same target. Shock waves are generated by exploding wire arrays driven by a high-voltage pulsed power system at beamline ID19 of the European Synchrotron Radiation Facility, delivering currents up to 130kA with rise times of 0.35 and 0.55 µs to the cylindrical and semicylindrical wire loads, respectively. X-ray radiography is conducted at a pulse repetition rate of 5.68 MHz using two synchronised high-speed cameras. Numerical hydrodynamic simulations are performed using a compressible multiphase Navier–Stokes solver. A Gilmore-type model for compressible cylindrical bubble pulsation provides an independent analytical estimate of the interface evolution. In the cylindrical SW configuration, the bubble collapse in experiments exhibits Richtmyer–Meshkov instability spikes. The cylindrically converging shock is analysed with Guderley’s solution and Whitham’s approximation using a real-gas equation of state, predicting Mach 14.1 near the focus. In the semicylindrical configuration, momentum focuses into a single supersonic jet with a speed of 885 ± 30 m s−1, producing localised high-pressure regions, coherent vortices and complex internal Mach reflections. Experiments, simulations and theory are consistent in collapse time, interface motion and overall flow dynamics.

Place, publisher, year, edition, pages
Cambridge University Press (CUP) , 2026. Vol. 1033, article id A29
Keywords [en]
bubble dynamics, gas/liquid flow, shock waves
National Category
Fluid Mechanics
Identifiers
URN: urn:nbn:se:kth:diva-381611DOI: 10.1017/jfm.2026.11472ISI: 001743494300001Scopus ID: 2-s2.0-105036891237OAI: oai:DiVA.org:kth-381611DiVA, id: diva2:2061485
Note

QC 20260521

Available from: 2026-05-21 Created: 2026-05-21 Last updated: 2026-05-21Bibliographically approved

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Hernandez Garcia, FrancescBhardwaj, SourabhRojas Mata, SebastianApazidis, NicholasLiverts, Michael

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