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Influence of Two-Phase Thermocapillary Flow on Cryogenic Liquid Retention in Microscopic PoresPrevious experiments indicate that the bubble point pressure of spacecraft liquid hydrogen acquisition devices is reduced substantially when the ullage is pressurized with heated hydrogen vapor. The objective is to determine whether the two-phase thermocapillary convection arising from thermodynamic non-equilibrium along the porous surfaces of such devices could lead to this observed degradation in retention performance. We also examine why retention capability appears to be unaffected by pressurization with heated helium or direct heating through the porous structure. Computational assessments based on coupled solution of the flowfield and liquid free surface indicate that for highly wetting fluids in small pores, dynamic pressure and vapor recoil dictate surface morphology and drive meniscus deformation. With superheating, the two terms exert the same influence on curvature and promote mechanical equilibrium, but with subcooling, the pressure distribution produces a suction about the pore center-line that degrades retention. This result points to thermocapillary-induced deformation arising from condensation as the cause for retention loss. It also indicates that increasing the level of non-equilibrium by reducing accommodation coefficient restricts deformation and explains why retention failure does not occur with direct screen heating or helium pressurization.
Document ID
19970001817
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Schmidt, G. R.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Nadarajah, A.
(Alabama Univ. Huntsville, AL United States)
Chung, T. J.
(Alabama Univ. Huntsville, AL United States)
Karr, G. R.
(Alabama Univ. Huntsville, AL United States)
Date Acquired
August 17, 2013
Publication Date
January 1, 1994
Publication Information
Publisher: American Inst. of Aeronautics and Astronautics
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-202588
NAS 1.26:202588
AIAA Paper 94-0836
Meeting Information
Meeting: Aerospace Sciences
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
97N11586
Distribution Limits
Public
Copyright
Public Use Permitted.
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