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contributor authorBellur, Kishan
contributor authorHussey, Daniel
contributor authorJacobson, David
contributor authorLamana, Jacob
contributor authorMedici, Ezequiel
contributor authorHermanson, James
contributor authorAllen, Dr. Jeffrey S.
contributor authorChoi, Chang Kyoung
date accessioned2019-02-28T11:00:29Z
date available2019-02-28T11:00:29Z
date copyright2/16/2018 12:00:00 AM
date issued2018
identifier issn0022-1481
identifier otherht_140_03_030904.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4251664
description abstractNeutron imaging enables direct visualization of evaporation and condensation of cryogenic propellants in metal containers such as aluminum and stainless steel. CFD models of propellant behaviors inside the large tanks have shown that a thin liquid film is formed along the interior surface, but this had not been verified experimentally. In the present study, neutron imaging is used to study evaporation and condensation rates of liquid methane inside a cylindrical 10 mm, Al 6061 cell. The liquid meniscus is clearly shown, but the spatial resolution is insufficient to directly image thin liquid films that may be on the interior surface. Optical density (neutron attenuation) analysis enables quantitative measurements of these liquid films. An optical density image is formed by removing the background noise and normalizing the liquid image with that of the empty cell. Optical densities are then transformed into a liquid transmission thickness using the Beer-Lambert law. This technique enables measurement of film thicknesses smaller than the spatial resolution of the imaging system. The above graphic shows an optical density image during condensation of methane and the corresponding horizontal scan which suggests that a 11 μm film exists on the wall. The images indicate that methane undergoes film-wise condensation and is perfectly wetting to aluminum.These experiments were conducted at the NIST Center for Neutron Research in the Neutron Imaging Facility and the relevant work is supported by an Early stage Innovations Grant from NASA's Space Technology Research Grants Program (Grant # NNX14AB05G).
publisherThe American Society of Mechanical Engineers (ASME)
titleNeutron attenuation analysis of cryogenic propellants
typeJournal Paper
journal volume140
journal issue3
journal titleJournal of Heat Transfer
identifier doi10.1115/1.4039169
journal fristpage30904
journal lastpage030904-1
treeJournal of Heat Transfer:;2018:;volume( 140 ):;issue: 003
contenttypeFulltext


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