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Simulations of Cryogenic Line Chilldown with Advanced Sub-Grid Wall Boiling Models A meso-scale model developed at MIT [2][11] for boiling processes in water was adapted for cryogens and demonstrated for chilldown of propellant transfer lines in both liquid nitrogen and hydrogen. The sub-grid boiling model accurately captures the contributions to heat transfer from the generation of bubble nuclei, growth, and interaction of the bubbles in the microlayer as well as quenching of the boiling surface following bubble departure. It was adapted for cryogenic fluids using thermodynamic scaling concepts taking into account non-dimensional pressures and temperatures that are scaled by the corresponding critical values for the fluid. The boiling model was demonstrated for line chilldown in liquid nitrogen (Darr et al. [6]). The predicted wall temperature at which quenching occurs was close to the test data while the slope of the temperature curve after quenching is initiated, showing a steeper variation than the test data. Simulations were also performed for liquid hydrogen by simulating experiments of Hartwig et al. [7]. Chilldown times in liquid hydrogen are much more rapid due to higher heat transfer in the film boiling regime and accounting for the higher turbulence levels were found to be important. Furthermore, at the much lower fluid temperatures in liquid hydrogen flows, accounting for the variable thermal properties of the solid material is critical and has a dramatic impact on the quench times. The need for additional studies to better understand the evolution of the quench front in liquid hydrogen was noted.
Document ID
20230018224
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Vineet Ahuja
(Combustion Research and Flow Technology (United States) Bedminster, United States)
Ashvin Hosangadi
(Combustion Research and Flow Technology (United States) Bedminster, United States)
Tim Weathers
(Combustion Research and Flow Technology (United States) Bedminster, United States)
Emilio Baglietto
(Massachusetts Institute of Technology Cambridge, United States)
Justin Pesich
(Glenn Research Center Cleveland, United States)
Mohammad Kassemi
(Case Western Reserve University Cleveland, Ohio, United States)
Date Acquired
December 14, 2023
Subject Category
Fluid Mechanics and Thermodynamics
Meeting Information
Meeting: AIAA SciTech Forum and Exposition
Location: Orlando, FL
Country: US
Start Date: January 8, 2024
End Date: January 12, 2024
Sponsors: American Institute of Aeronautics and Astronautics, Lockheed Martin (United States)
Funding Number(s)
WBS: 448428.05.04.22
CONTRACT_GRANT: 80NSSC20C0195
CONTRACT_GRANT: 80NSSC21C0619
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
Computational Fluid Dynamics
Flow Boiling
Cryogenics
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