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Effect of Nonlinear Mixing on Electrospray Propulsion Predictions

2020; American Institute of Aeronautics and Astronautics; Volume: 37; Issue: 1 Linguagem: Inglês

10.2514/1.b38045

1533-3876

Mitchell J. Wainwright, Joshua L. Rovey,

Enzyme Catalysis and Immobilization

No AccessTechnical NotesEffect of Nonlinear Mixing on Electrospray Propulsion PredictionsMitchell J. Wainwright and Joshua L. RoveyMitchell J. WainwrightMissouri University of Science and Technology, Rolla, Missouri 65409*Graduate Research Assistant, Department of Mechanical and Aerospace Engineering; . Student Member AIAA.Search for more papers by this author and Joshua L. RoveyUniversity of Illinois Urbana-Champaign, Urbana, Illinois 61801†Associate Professor, Department of Aerospace Engineering, 317 Talbot Laboratory, 104 South Wright Street; . Associate Fellow AIAA.Search for more papers by this authorPublished Online:22 Oct 2020https://doi.org/10.2514/1.B38045SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Chatel G., Pereira J. F. B., Debbeti V., Wang H. and Rogers R. D., “Mixing Ionic Liquids—‘Simple Mixtures’ or ‘Double Salts’?” Green Chemistry, Vol. 16, No. 4, 2014, pp. 2051–2083. 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L., Prince B., Miller S. and Bemish R., “Electrospray of an Energetic Ionic Liquid Monopropellant for Multi-Mode Micropropulsion Applications,” 51st AIAA/SAE/ASEE Joint Propulsion Conference, AIAA Paper 2015-4011, 2015. LinkGoogle Scholar Previous article Next article FiguresReferencesRelatedDetailsCited byMultiscale modeling of fragmentation in an electrospray plumeJournal of Applied Physics, Vol. 130, No. 18 What's Popular Volume 37, Number 1January 2021 CrossmarkInformationCopyright © 2020 by Mitchell J. Wainwright. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. 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. TopicsComputational Fluid DynamicsFluid DynamicsFluid Flow PropertiesIon ThrusterMolecular DynamicsNumerical AnalysisNumerical InterpolationPropellantPropulsion and PowerSpacecraft Propulsion KeywordsPropulsionPropellantSurface TensionDielectric PropertiesVapour PressureLinear InterpolationMolecular DynamicsColloid ThrustersMass Flow RateAcknowledgmentsThis work was supported by the NASA Marshall Space Flight Center (NASA grant NNM15AA09A), the Air Force University Nano-satellite Program (Utah State University Research Foundation, grant CP0039814), NASA Goddard (through the NASA Undergraduate Student Instrument Project grant NNX16AI85A), and the University of Missouri Fast Track Program (FastTrack-16003R). M. Wainwright thanks the Department of Education for GAANN Fellowship P200A150309, Missouri Space Grant Consortium, Yifu Long for help with surface tension measurements and Maser and Riggins for help with the manuscript.PDF Received18 March 2020Accepted14 September 2020Published online22 October 2020