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Modeling of Particle Transport and Impact in Transient, Multiphase Oxidizer-Rich Environments Using Computational Fluid Dynamics and Lagrangian Particle TrackingParticle impacts from foreign object debris (FOD) in an oxidizer-rich environment have been shown to be a credible and significant risk for ignition and failure of components and vehicles. The risk of particle ignition is dependent on many factors, including particle impact velocity/energy and fluid composition (i.e. fluid phase, species presence, and state). Prediction of particle transport and particle impacts in relevant environments, including transient, multiphase flows, is important for assessing the risk and avoiding repeated expensive system level tests. The capability to model both the fluid dynamics and particle transport in complex three-dimensional geometries and multiphase environments has been developed at Marshall Space Flight Center (MSFC) in the propulsion fluid dynamic branch (ER42) by utilizing computational fluid dynamics (CFD) simulations and Lagrangian particle tracking. Using CFD tools, including density-based Loci/CHEM with a cavitation model and pressure-based Loci/STREAM with a volume of fluids model, MSFC/ER42 has provided particle impact predictions to multiple projects for oxidizer compatibility assessments. Simulations of transient, multiphase environments such as liquid slugs flowing through tubing and cavitating flow in valves have been completed alongside one-way coupled Lagrangian particle tracking to predict particle impacts.
Document ID
20230005389
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
M.V. Fischels
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
M.J. Brunhart
(Jacobs (United States) Dallas, Texas, United States)
A.J. Rips
(Tuskegee University Tuskegee, Alabama, United States)
H.Q. Yang
(CFD Research Corporation (United States) Huntsville, Alabama, United States)
J.S. West
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
B.R. Williams
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Date Acquired
April 12, 2023
Subject Category
Fluid Mechanics And Thermodynamics
Computer Programming and Software
Meeting Information
Meeting: Particle Impact Ignition in Oxygen Enriched Environments Workshop
Location: Las Cruces, NM
Country: US
Start Date: April 25, 2023
End Date: April 26, 2023
Sponsors: National Aeronautics and Space Administration, American Society For Testing and Materials
Funding Number(s)
WBS: 484997.01.07.02.03
CONTRACT_GRANT: 80MSFC18C0011
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Professional Review
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