Two-dimensional modeling of capillary liquid flow in a thin annulus
Abstract
A model for the flow in a thin annular cylinder such as a spacecraft fuel tank or cooling system, is developed. The model assumes that only azimuthal and axial directions are important; the flow in radial direction is negligible. The model uses the Euler equations, solved numerically by the code ANVOF. Examples to illustrate the method include one in which a tank performs a slew maneuver and the influence (i.e., force, torque, location of the center of mass) of the liquid on the tank is calculated.
- Publication:
-
NASA STI/Recon Technical Report N
- Pub Date:
- August 1984
- Bibcode:
- 1984STIN...8713684V
- Keywords:
-
- Capillary Flow;
- Liquid Filled Shells;
- Liquid Sloshing;
- Mathematical Models;
- Two Dimensional Models;
- Concentric Cylinders;
- Euler Equations Of Motion;
- Incompressible Flow;
- Interfacial Tension;
- Satellite Attitude Control;
- Slewing;
- Space Commercialization;
- Spacelab Payloads;
- Weightlessness;
- Fluid Mechanics and Heat Transfer