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Dewetting behaviour of liquid bridges stretched by an accelerated plate

Brulin, Sebastian ; Roisman, Ilia ; Tropea, Cameron (2019)
Dewetting behaviour of liquid bridges stretched by an accelerated plate.
14th Triennial International Conference on Liquid Atomization and Spray Systems. Chicago, IL (22.07.-26.07.2018)
Konferenzveröffentlichung, Zweitveröffentlichung

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Kurzbeschreibung (Abstract)

Liquid bridge stretching is of interest for a wide field of industrial applications like printing and coating, but also for the functioning of aircraft engines because of its importance in the process of ice crystal icing. In the present experimental study, the focus lies on describing the geometry of the liquid bridge during the stretching process with respect to midpoint diameter, contact line diameter and contact angle for constant accelerations from 10m/s 2 up to 180m/s 2 . The observed evolution of the dynamic contact angle is described as a function of the capillary number. For the early phase of the stretching process relations for the curvature and midpoint diameter are proposed.

Typ des Eintrags: Konferenzveröffentlichung
Erschienen: 2019
Autor(en): Brulin, Sebastian ; Roisman, Ilia ; Tropea, Cameron
Art des Eintrags: Zweitveröffentlichung
Titel: Dewetting behaviour of liquid bridges stretched by an accelerated plate
Sprache: Englisch
Publikationsjahr: 29 November 2019
Ort: Darmstadt
Publikationsdatum der Erstveröffentlichung: 2018
Verlag: Institute for Liquid Atomization and Spray Systems
Buchtitel: ICLASS 2018, 14th Triennial International Conference on Liquid Atomization and Spray Systems, Chicago, IL, USA, July 22-26, 2018
Veranstaltungstitel: 14th Triennial International Conference on Liquid Atomization and Spray Systems
Veranstaltungsort: Chicago, IL
Veranstaltungsdatum: 22.07.-26.07.2018
URL / URN: https://tuprints.ulb.tu-darmstadt.de/9279
Zugehörige Links:
Kurzbeschreibung (Abstract):

Liquid bridge stretching is of interest for a wide field of industrial applications like printing and coating, but also for the functioning of aircraft engines because of its importance in the process of ice crystal icing. In the present experimental study, the focus lies on describing the geometry of the liquid bridge during the stretching process with respect to midpoint diameter, contact line diameter and contact angle for constant accelerations from 10m/s 2 up to 180m/s 2 . The observed evolution of the dynamic contact angle is described as a function of the capillary number. For the early phase of the stretching process relations for the curvature and midpoint diameter are proposed.

URN: urn:nbn:de:tuda-tuprints-92792
Sachgruppe der Dewey Dezimalklassifikatin (DDC): 600 Technik, Medizin, angewandte Wissenschaften > 620 Ingenieurwissenschaften und Maschinenbau
Fachbereich(e)/-gebiet(e): 16 Fachbereich Maschinenbau
16 Fachbereich Maschinenbau > Fachgebiet Strömungslehre und Aerodynamik (SLA)
Hinterlegungsdatum: 19 Jun 2024 14:56
Letzte Änderung: 19 Jun 2024 14:56
PPN: 457512032
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