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Self-Pressurization and Spray Cooling Simulations of the Multipurpose Hydrogen Test Bed (MHTB) Ground-Based ExperimentThis paper presents a CFD (computational fluid dynamics) model for simulating the self-pressurization of a large scale liquid hydrogen storage tank. In this model, the kinetics-based Schrage equation is used to account for the evaporative and condensing interfacial mass flows. Laminar and turbulent approaches to modeling natural convection in the tank and heat and mass transfer at the interface are compared. The flow, temperature, and interfacial mass fluxes predicted by these two approaches during tank self-pressurization are compared against each other. The ullage pressure and vapor temperature evolutions are also compared against experimental data obtained from the MHTB (Multipuprpose Hydrogen Test Bed) self-pressurization experiment. A CFD model for cooling cryogenic storage tanks by spraying cold liquid in the ullage is also presented. The Euler- Lagrange approach is utilized for tracking the spray droplets and for modeling interaction between the droplets and the continuous phase (ullage). The spray model is coupled with the VOF (volume of fluid) model by performing particle tracking in the ullage, removing particles from the ullage when they reach the interface, and then adding their contributions to the liquid. Droplet ullage heat and mass transfer are modeled. The flow, temperature, and interfacial mass flux predicted by the model are presented. The ullage pressure is compared with experimental data obtained from the MHTB spray bar mixing experiment. The results of the models with only droplet/ullage heat transfer and with heat and mass transfer between the droplets and ullage are compared.
Document ID
20150000249
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Kartuzova, O.
(Apogee Engineering, LLC Colorado Springs, CO, United States)
Kassemi, M.
(Case Western Reserve Univ. Cleveland, OH, United States)
Agui, J.
(NASA Glenn Research Center Cleveland, OH, United States)
Moder, J.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
January 8, 2015
Publication Date
July 28, 2014
Subject Category
Propellants And Fuels
Engineering (General)
Report/Patent Number
GRC-E-DAA-TN16496
Meeting Information
Meeting: AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Location: Cleveland, OH
Country: United States
Start Date: July 28, 2014
End Date: July 30, 2014
Sponsors: American Society of Mechanical Engineers, American Society for Engineering Education, Society of Automotive Engineers, Inc., American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 095240.04.12.02.03
CONTRACT_GRANT: NNC08BA08B
CONTRACT_GRANT: NNC08BA05B
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
cryogenic fluid storage
mass transfer
active control
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