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Influence of Two-Phase Thermocapillary Flow on Liquid Retention in Microscopic PoresAn important feature of screened propellant acquisition devices is the retention capability or maximum maintainable pressure difference across the porous barrier separating the liquid and gas. Previous experiments with liquid hydrogen showed a marked reduction in retention when the tank containing the device was pressurized with hydrogen vapor. These tests, however did not indicate any appreciable degradation in retention with helium pressurization or direct heating through the screen. The objective of this article is to determine if the thermocapillary convection arising from phase change in the microscopic pores of such screens could cause these disparities in performance. A numerical model of flow in a single pore suggests that the thermocapillary-induced gradient in liquid pressure along the surface can strongly affect surface morphology. In an evaporative environment, this gradient exerts a stabilizing influence on surface curvature, and preserves the momentum balance between the liquid and gas. With condensation, it causes a force imbalance and a destabilizing suction in the middle of the pore that reduces retention. Results also indicate that introducing an inert gas, such as helium, suppresses this retention loss mechanism by lowering thermocapillary circulation and its associated interfacial pressure gradient.
Document ID
19970011866
Acquisition Source
Marshall Space Flight Center
Document Type
Reprint (Version printed in journal)
Authors
Schmidt, George R.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Nadarajah, Arun
(Alabama Univ. Huntsville, AL United States)
Chung, T. J.
(Alabama Univ. Huntsville, AL United States)
Karr, Gerald R.
(Alabama Univ. Huntsville, AL United States)
Date Acquired
August 17, 2013
Publication Date
March 1, 1995
Publication Information
Publication: Journal of Thermophysics and Heat Transfer
Publisher: American Inst. of Aeronautics and Astronautics, Inc.
Volume: 9
Issue: 1
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.15:111817
NASA-TM-111817
AIAA Paper 94-0836
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Reno, NV
Country: United States
Start Date: January 10, 1994
End Date: January 13, 1994
Sponsors: American Inst. of Aeronautics and Astronautics
Accession Number
97N70855
Distribution Limits
Public
Copyright
Public Use Permitted.
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