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Joule-Thomson Cryogenic Nitrogen Orifice FlowsThe Joule-Thomson Effect involves the expansion of a fluid through a throttling device, often a simple orifice, resulting in a change in the fluid's temperature. It has been leveraged in the design and analysis of Thermodynamic Vent Systems and integrated into injector designs for cryogenic no-vent fill tank-to-tank transfer testing. There is a scarcity of comprehensive data available to model the phenomenon effectively using tools such as GFSSP for cryogenic nitrogen flows. This experiment aims to model the Joule-Thomson effect of liquid nitrogen through seven traditionally manufactured, sharp-edged orifices manufactured by O’Keefe and three additively manufactured (AM) orifices manufactured by Cumberland Additive. The traditional orifice sizes were 0.016, 0.02, 0.024, 0.032, 0.037, and 0.04 inch in diameter. The three additive orifices had diameters with target/nominal sizes equal to the 0.016, 0.024, and 0.04 inch O’Keefe orifices. However, the actual diameters of the AM orifices were found to be 0.014, 0.024, and 0.035 inches due to additive manufacturing restrictions.
Water was flowed through the orifices to verify that their flow coefficients matched published values and to establish flow coefficients for the AM orifices. Liquid nitrogen was flowed through the orifices in a separate test apparatus. The liquid nitrogen started as a subcooled liquid upstream of the orifice and transitioned into a two-phase gas-liquid mixture after passing through each orifice. The upstream pressure was set to 29 psia, 34 psia, 39 psia, and/or 42 psia or 44 psia. The pressure, temperature, and flow rate were measured upstream and downstream of the orifice for three trials at each set point. The average volumetric flow rate and Joule-Thomson Coefficients were calculated from this data. The AM orifices and traditionally manufactured orifices displayed similar results. This data will refine the dataset GFSSP uses to model the J-T Effect more accurately.
Document ID
20240015559
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Ebony M. Bland
(Marshall Space Flight Center Redstone Arsenal, United States)
Hannah E. Cherry
(Marshall Space Flight Center Redstone Arsenal, United States)
Nicole M. Vaughn
(Marshall Space Flight Center Redstone Arsenal, United States)
Kevin W. Pedersen
(Marshall Space Flight Center Redstone Arsenal, United States)
Mason Lebakken
(Embry-Riddle Aeronautical Univ. Daytona Beach, FL, United States)
L. Catherine Potts
(Florida State University Tallahassee, United States)
Date Acquired
December 4, 2024
Subject Category
Propellants and Fuels
Fluid Mechanics and Thermodynamics
Meeting Information
Meeting: AIAA SciTech Forum and Exposition
Location: Orlando, FL
Country: US
Start Date: January 6, 2025
End Date: January 10, 2025
Sponsors: American Institute of Aeronautics and Astronautics AIAA
Funding Number(s)
WBS: 981698.01.01.62.40.06
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Peer Committee
Keywords
Joule-Thomson
Cryogenic
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