Modeling Self-Pressurization and Spray Bar Pressure Control of a Cryogenic Storage Tank in Normal GravityThis paper presents Computational Fluid Dynamics (CFD) models for simulating self-pressurization and spray bar cooling processes in a large-scale liquid hydrogen storage tank under normal gravity. The self-pressurization model utilizes the kinetics-based Schrage equation with the Volume-Of-Fluid (VOF) model to account for the evaporative and condensing interfacial mass fluxes. It uses a laminar approach to model natural convection and compares the pressures and temperatures predicted by the CFD model with experimental data from the Multipurpose Hydrogen Test Bed (MHTB) self-pressurization experiment. Additionally, the predicted interfacial mass flux is presented. A CFD model for simulating pressure control using a spray bar is also presented. An Eulerian-Lagrangian approach models the interactions between the discrete droplets and the continuous ullage phase. The spray model is coupled with the VOF model by tracking particles in the ullage, removing particles from the ullage when they reach the interface, and then adding their contributions to the liquid. The T-sat model is used to calculate the droplet-ullage heat and mass transfer. In this model, droplets warm up to the saturation temperature corresponding to the ullage vapor pressure thereafter evaporating while remaining at the saturation temperature. The tank pressure, vapor, and liquid temperature evolutions are validated against data from the MHTB spray bar mixing experiment.
Document ID
20240006408
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
Self-PressurizationComputational Fluid DynamicsCryogenic PropellantsSpray-Bar Pressure Control