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      Outgassing Characteristics from Oxygen Dissolved in JP-8 During Depressurization

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          Abstract

          Outgassing of oxygen from fuel is an important phenomenon affecting the ullage oxygen concentration of aircraft fuel tanks, which is a critical operating parameter associated with the risk of explosions due to hazards such as electric sparks or combat damage. Knowledge of the outgassing characteristics of specific fuels in their operational environment is important to fuel system designers. Although the factors affecting the evolution rate of dissolved gases from solution, such as pressure, temperature, and agitation, have been characterized to some extent, the effect of bubble generation on the bulk rate of outgassing to the ullage space has not been well described in the literature. The motivation for the present work was to study the effect of bubbles naturally induced by fuel pumps on the outgassing of JP-8 during depressurizations that are typical for climb and high-altitude cruise. An experimental fuel tank model was developed that included visualization windows, oxygen measurements in the fuel and ullage, and a vacuum system enabling controlled depressurization down to 0.1 atm. Significant differences between bubble-up and diffusion-driven outgassing are evident in the analysis of oxygen concentration trends with time under various test conditions. The ullage oxygen volume fraction is significantly increased during depressurization when agitation is accompanied by small bubbles, in comparison to quiet conditions. Ullage washing before depressurization affects the initial state but not the overall transient characteristics, regardless of whether agitation is applied.

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          Most cited references8

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          Dissolved air flotation

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            Gas Dissolution, Release, and Bubble Formation in Flotation Systems

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              Vulnerability Methodology and Protective Measures for Aircraft Fire and Explosion Hazards, Volume III, On-Board Inert Gas Generating System (OBIGGS) Studies, Part 2: Fuel Scrubbing and Oxygen Evolution Tests

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                Author and article information

                Journal
                jpp
                Journal of Propulsion and Power
                J. Propulsion
                American Institute of Aeronautics and Astronautics
                1533-3876
                27 January 2020
                May–June 2020
                : 36
                : 3
                : 446-452
                Affiliations
                Korea Aerospace Industries, Sacheon 52529, Gyeongnam, Republic of Korea
                Lockheed Martin Aeronautics, Fort Worth, Texas 76108
                Author notes
                [*]

                Senior Research Engineer.

                [†]

                Computational Fluid Dynamics Specialist, Engineering & Technology Senior Staff. Senior Member AIAA.

                Article
                B37749 B37749
                10.2514/1.B37749
                3fe98c79-42c2-488f-99c7-b9d1fe4b70fa
                Copyright © 2019 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-3876 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.
                History
                : 17 July 2019
                : 17 December 2019
                : 21 December 2019
                Page count
                Figures: 9, Tables: 3
                Funding
                Funded by: Defense Acquisition Program Administration(DAPA)
                Award ID: 4747000155
                Categories
                Full-Length Papers

                Engineering,Physics,Mechanical engineering,Space Physics
                Engineering, Physics, Mechanical engineering, Space Physics

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