Journalartikel
Autorenliste: Schwabe, D
Jahr der Veröffentlichung: 2005
Zeitschrift: Physics of Fluids
Bandnummer: 17
Heftnummer: 11
ISSN: 1070-6631
DOI Link: https://doi.org/10.1063/1.2135805
Verlag: American Institute of Physics
Abstract:
A 2 cSt silicone oil (Pr=28) liquid bridge of 15.0 mm length L and 3.0 mm radius r (aspect ratio A=L/r=5) was established under microgravity during the flight of the sounding rocket MAXUS-4. Four different temperature differences Delta T=7, 9, 10, and 12 K were applied between the ends, each for sufficient time to reach steady-state thermocapillary flow conditions. The aim of the experiment-to observe the onset of hydrothermal waves and to measure their features such as the wave phase speed and the angle between the wave vector and the applied temperature gradient-was reached. We used microgravity in this experiment in a twofold manner: (1) a liquid bridge with A=5 can be established only under microgravity; (2) it was possible to study hydrothermal waves without the influence of gravity and without the aspect ratio restrictions at normal gravity. (c) 2005 American Institute of Physics.
Zitierstile
Harvard-Zitierstil: Schwabe, D. (2005) Hydrothermal waves in a liquid bridge with aspect ratio near the Rayleigh limit under microgravity, Physics of Fluids, 17(11), Article 112104. https://doi.org/10.1063/1.2135805
APA-Zitierstil: Schwabe, D. (2005). Hydrothermal waves in a liquid bridge with aspect ratio near the Rayleigh limit under microgravity. Physics of Fluids. 17(11), Article 112104. https://doi.org/10.1063/1.2135805
Schlagwörter
INSTABILITIES; Layers; MARANGONI NUMBER; OSCILLATORY THERMOCAPILLARY CONVECTION; STEADY