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Validation of a Two-Phase CFD Model for Autogenous Pressurization and ExpulsionThis paper presents a two-phase computational fluid dynamics (CFD) model for simulating autogenous pressurization and expulsion in a cryogenic liquid hydrogen storage tank, utilizing a volume-of-fluid (VOF) approach combined with the kinetics-based Schrage equation to accurately capture the phase boundary and interfacial heat, mass, and momentum transfer between liquid and vapor phases. The model is validated against experimental data from NASA's K-site tank facility, specifically experimental case 225, which involved pressurization and controlled expulsion of liquid hydrogen. Various turbulence models are evaluated to assess their influence on model accuracy. The CFD simulations successfully replicate key thermodynamic behaviors observed during the experiments, including pressure evolution, temperature profiles, and phase-change dynamics at the vapor-liquid interface. The predicted tank pressures, temperatures, and pressurant requirements agree with experimental data, with pressurant mass predictions within 16\% of observed values. This study highlights the importance of selecting appropriate turbulence models to accurately simulate complex flow and heat transfer phenomena during tank pressurization and expulsion. By enhancing the accuracy and reliability of CFD models for liquid hydrogen under cryogenic conditions, this research contributes to developing efficient cryogenic propellant management strategies for future space missions.
Document ID
20240014419
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Steven Soriano
(HX5 (United States) Fort Walton Beach, Florida, United States)
Olga Kartuzova
(Case Western Reserve University Cleveland, United States)
Mohammad Kassemi
(Case Western Reserve University Cleveland, United States)
Daniel Hauser
(Glenn Research Center Cleveland, United States)
Date Acquired
November 13, 2024
Subject Category
Propellants and Fuels
Meeting Information
Meeting: AIAA SciTech Forum
Location: Orlando, FL
Country: US
Start Date: January 6, 2025
End Date: January 10, 2025
Sponsors: American Institute of Aeronautics and Astronautics, Lockheed Martin (United States), Northrop Grumman (United States)
Funding Number(s)
WBS: 633369.07.01.04.22
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
Computational Fluid Dynamics
Cryogenic Propellants
Autogenous Pressurization
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