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CFD-Assisted Nodal Modeling of Sloshing in a Cryogenic Propellant Tank During autogenous pressurization, tank sloshing causes a significant increase in pressurant consumption to maintain constant ullage pressure during draining of the tank. This increase in pressurant consumption is caused by a significant increase in condensation at the liquid-vapor interface. Sloshing strongly affects the liquid side heat transfer coefficient and thereby the condensation rate. Traditionally, sloshing is modeled by CFD code using the VOF (Volume of Fluid) method to track the liquid vapor interface during sloshing. CFD calculations require a very fine grid to accurately compute the heat and mass transfer at the interface. Therefore, computations are time consuming and prohibit performing many parametric studies often needed during the design of a new system. This paper describes an alternative approach by developing a CFD-assisted nodal model to predict system parameters more economically with reasonable accuracy. In this approach, a multi-node model of tank pressurization was developed using GFSSP. A multi-node model was needed to account for stratification. The model computes heat and mass transfer at the interface to calculate the condensation rate. The liquid side heat transfer is computed using the parameters of sloshing dynamics such as frequency, wave amplitude, and interface area. The parameters of sloshing dynamics are computed by the CFD code LOCI-Stream. The model predictions were compared with test data for several cases.
Document ID
20260007790
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Alok Majumdar
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Andre LeClair
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Ramon Lopez Otero
(CFD Research Corp. Huntsville, AL, United States)
Jacob Brodnick
(Marshall Space Flight Center Redstone Arsenal, United States)
Date Acquired
August 12, 2026
Publication Date
August 31, 2026
Publication Information
Subject Category
Spacecraft Design, Testing and Performance
Propellants and Fuels
Meeting Information
Meeting: Thermal Fluid Analysis Workshop Workshop (TFAWS 2026)
Location: Huntsville, AL
Country: US
Start Date: August 31, 2026
End Date: September 4, 2026
Sponsors: NASA Marshall Space Flight Center
Funding Number(s)
WBS: 633369.07.01.04.62
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Cryogenic Tank Sloshing
Nodal Model
Condensation
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