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Modeling of Water Injection into a VacuumA loosely coupled two-phase vacuum water plume model has been developed. This model consists of a source flow model to describe the expansion of water vapor, and the Lagrangian equations of motion for particle trajectories. Gas/Particle interaction is modeled through the drag force induced by the relative velocities. Particles are assumed traveling along streamlines. The equations of motion are integrated to obtain particle velocity along the streamline. This model has been used to predict the mass flux in a 5 meter radius hemispherical domain resulting from the burst of a water jet of 1.5 mm in diameter, mass flow rate of 24.2 g/s, and stagnation pressure of 21.0 psia, which is the nominal Orbiter water dump condition. The result is compared with an empirical water plume model deduced from a video image of the STS-29 water dump. To further improve the model, work has begun to numerically simulate the bubble formation and bursting present in a liquid stream injected into a vacuum. The technique of smoothed particle hydrodynamics was used to formulate this simulation. A status and results of the on-going effort are presented and compared to results from the literature.
Document ID
19970040115
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Alred, John W.
(Hernandez Engineering, Inc. Houston, TX United States)
Smith, Nicole L.
(Lockheed Martin Corp. Houston, TX United States)
Wang, K. C.
(Lockheed Martin Corp. Houston, TX United States)
Lumpkin, Forrest E.
(NASA Johnson Space Center Houston, TX United States)
Fitzgerald, Steven M.
(NASA Johnson Space Center Houston, TX United States)
Date Acquired
August 17, 2013
Publication Date
September 1, 1997
Publication Information
Publication: Proceedings of the Eighth Annual Thermal and Fluids Analysis Workshop: Spacecraft Analysis and Design
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
97N31273
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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