Results are reported of the Surface Tension Driven Convection Experiment (STDCE) aboard the USML-1 Spacelab, which was launched on June 25, 1992. In the experiment, 10 cSt silicone oil was placed in an open 10-cm-dia circular container, which was 5 cm deep. The fluid was heated either by a cylinderical heater (1.11 cm diameter) located along the container centerline or by a CO2 laser beam to induce thermocapillary flow. Several thermistor probes were placed in the fluid to measure the temperature distribution. The temperature distribution along the liquid-free surface was measured by an infrared imager. Tests were conducted over a range of heating powers, laser-beam diameters, and free surface shapes. An extensive numerical modeling of the flow was conducted in conjunction with the experiments. Some results of the temperature measurements with flat free surfaces are presented in this paper and they are shown to agree well with the numerical predictions.
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A Thermocapillary Convection Experiment in Microgravity
Y. Kamotani,
Y. Kamotani
Department of Mechanical and Aerospace Engineering, Case Western Reserve University, Cleveland, OH 44106
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S. Ostrach,
S. Ostrach
Department of Mechanical and Aerospace Engineering, Case Western Reserve University, Cleveland, OH 44106
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A. Pline
A. Pline
NASA Lewis Research Center, Cleveland, OH 44135
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Y. Kamotani
Department of Mechanical and Aerospace Engineering, Case Western Reserve University, Cleveland, OH 44106
S. Ostrach
Department of Mechanical and Aerospace Engineering, Case Western Reserve University, Cleveland, OH 44106
A. Pline
NASA Lewis Research Center, Cleveland, OH 44135
J. Heat Transfer. Aug 1995, 117(3): 611-618 (8 pages)
Published Online: August 1, 1995
Article history
Received:
October 1, 1993
Revised:
October 1, 1994
Online:
December 5, 2007
Connected Content
A companion article has been published:
On Fast-Response Probes: Part 2—Aerodynamic Probe Design Studies
Citation
Kamotani, Y., Ostrach, S., and Pline, A. (August 1, 1995). "A Thermocapillary Convection Experiment in Microgravity." ASME. J. Heat Transfer. August 1995; 117(3): 611–618. https://doi.org/10.1115/1.2822621
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