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Validation of a Two-Phase CFD Model for Autogenous Pressurization and ExpulsionThis paper presents a two-phase CFD model for tank pressurization and expulsion in a liquid hydrogen cryogenic storage tank. The model uses a Volume-of-Fluid approach combined with the Kinetics-based Schrage equation to capture the phase boundary and the associated interfacial heat, mass, and momentum transfer between the liquid and vapor regions. The CFD model is validated against expulsion data from the NASA K-Site tank experiment. Predicted tank pressures, temperatures, and pressurant requirements are compared with the experimental data to demonstrate the model’s accuracy.
Document ID
20240006400
Acquisition Source
Glenn Research Center
Document Type
Extended Abstract
Authors
Steven Soriano
(HX5, LLC)
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
May 17, 2024
Subject Category
Propellants and Fuels
Meeting Information
Meeting: AIAA SciTech Forum and Exposition
Location: Orlando, FL
Country: US
Start Date: January 6, 2025
End Date: January 10, 2025
Sponsors: Bastion Technologies, American Institute of Aeronautics and Astronautics, Lockheed Martin (United States)
Funding Number(s)
WBS: 448428.05.04.22
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
Autogenous Pressurization
Cryogenic Propellants
Computational Fluid Dynamics
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