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Numerical simulation of low gravity drainingA boundary value problem was solved numerically for a liquid that is assumed to be inviscid and incompressible, having a motion that is irrotational and axisymmetric, and having a constant (5 degrees) solid-liquid contact angle. The avoidance of excessive mesh distortion, encountered with strictly Lagrangian or Eulerian kinematics, was achieved by introducing an auxiliary kinematic velocity field along the free surface in order to vary the trajectories used in integrating the ordinary differential equations simulating the moving boundary. The computation of the velocity potential was based upon a nonuniform triangular mesh which was automatically revised to varying depths to accommodate the motion of the free surface. These methods permitted calculation of draining induced axisymmetric slosh through the many (or fractional) finite amplitude oscillations that can occur depending upon the balance of draining, gravitational, and surface tension forces. Velocity fields, evolution of the free surface with time, and liquid residual volumes were computed for three and one half decades of Weber number and for two Bond numbers, tank fill levels, and drain radii. Comparisons with experimental data are very satisfactory.
Document ID
19760019335
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bizzell, G. D.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Crane, G. E.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1976
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-135004
LMSC-D521581
Report Number: NASA-CR-135004
Report Number: LMSC-D521581
Accession Number
76N26423
Funding Number(s)
CONTRACT_GRANT: NAS3-17798
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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