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SINDA/FLUINT and Thermal Desktop Multi-Node Settled and Unsettled Propellant Tank Modeling of Zero Boil Off TestCryogenic propellant storage tank self-pressurization involves complex physical phenomena which are usually analytically modelled via complex multidimensional CFD (Computational Fluid Dynamics) codes. Unfortunately these codes, even when modelling axisymmetric domains, may take weeks or longer to obtain transient pressure and temperature information for relatively short periods of time (several seconds to several hours). Propellant tank storage end-to-end mission simulations can last a duration of days to weeks to months. Multi-node modelling of propellant tanks is a viable alternative to traditional CFD modelling and presents the advantage of greatly reduced run times on the order of hours and days compared to the weeks or longer for CFD codes. A multi-node model represents the fluid within the storage tank, as well as the storage tank itself, as a fluid-thermal network. This type of setup is not necessarily geometrically based. This can be accomplished using a commercial generalized fluid-thermal network code, such as SINDA/FLUINT (SF). The advantage of using a fluid-thermal network code like SF lies in its extensive ability to model the external environment of the storage tank through the graphical user interface, Thermal Desktop (TD). The total heat load into the tank may be a function of heaters and a complex radiative environment as well. Thermal Desktop may be used to address the detailed radiative environment of the tank as well as building a geometrically accurate depiction of the storage tank itself.
Document ID
20190031763
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Sakowski, Barbara
(NASA Glenn Research Center Cleveland, OH, United States)
Hauser, Daniel M.
(NASA Glenn Research Center Cleveland, OH, United States)
Kassemi, M.
(National Center for Space Exploration Research Cleveland, OH, United States)
Date Acquired
September 25, 2019
Publication Date
August 19, 2019
Subject Category
Propellants And Fuels
Report/Patent Number
GRC-E-DAA-TN72542
GRC-E-DAA-TN72598
Report Number: GRC-E-DAA-TN72542
Report Number: GRC-E-DAA-TN72598
Meeting Information
Meeting: AIAA/SAE/ASEE Joint Propulsion and Energy Forum and Exposition
Location: Indianapolis, IN
Country: United States
Start Date: August 19, 2019
End Date: August 22, 2019
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Funding Number(s)
CONTRACT_GRANT: NNC13BA10B
WBS: 448887.04.03.02
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
Thermal Desktop
SINDA/FLUENT
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