Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/93043
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dc.contributorDepartment of Mechanical Engineeringen_US
dc.creatorLiu, Yen_US
dc.creatorGuan, Ben_US
dc.creatorWen, CYen_US
dc.creatorShen, Hen_US
dc.date.accessioned2022-05-30T07:40:15Z-
dc.date.available2022-05-30T07:40:15Z-
dc.identifier.isbn9781624104633en_US
dc.identifier.urihttp://hdl.handle.net/10397/93043-
dc.language.isoenen_US
dc.rightsCopyright © 2017 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.en_US
dc.rightsThe following publication Liu, Y., Wen, C., Shen, H., & Guan, B. (2017). Investigation on Shock Induced Stripping Breakup Process of A Liquid Droplet. In 21st AIAA International Space Planes and Hypersonics Technologies Conference, 6-9 March 2017, Xiamen, China, AIAA 2017-2369 is available at https://doi.org/10.2514/6.2017-2369en_US
dc.titleInvestigation on shock induced stripping breakup process of a liquid dropleten_US
dc.typeConference Paperen_US
dc.identifier.doi10.2514/6.2017-2369en_US
dcterms.abstractStripping breakup process of a single liquid droplet under the impact of a planar shock wave is investigated both experimentally and numerically. The droplet breakup experiment is conducted in a horizontal shock tube and the evolution of the droplet is recorded by direct high-speed photography. The experimental images clearly illustrate the droplet interface evolution features from its early to relatively late stage. Compressible Euler equations are solved using an in-house inviscid upwind characteristic space-time conservation element and solution element (CE/SE) method coupled with the HLLC approximate Riemann solver. A reduced five-equation model is employed to demonstrate the air/liquid interface. Numerical results accurately reproduce the water column and axi-symmetric water droplet breakup processes in experiments. The present study confirms the validity of the present numerical method in solving the shock wave induced droplet breakup problem and elaborates the stripping breakup process numerically in a long period. Droplet inner flow pattern is depicted, based on which the drives of protrusions emerged on the droplet surface are clearly seen. The droplet deformation is proved to be determined by not only the outer air flow, but also the inner liquid flow.en_US
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitation21st AIAA International Space Planes and Hypersonics Technologies Conference, 6-9 March 2017, Xiamen, China, AIAA 2017-2369, Session: Hypersonic Fundamentals and History Xen_US
dcterms.issued2017-
dc.identifier.scopus2-s2.0-85085406311-
dc.relation.conference21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017en_US
dc.identifier.artnAIAA 2017-2369en_US
dc.description.validate202205 bchyen_US
dc.description.oaAccepted Manuscripten_US
dc.identifier.FolderNumberME-0924-
dc.description.fundingSourceRGCen_US
dc.description.fundingSourceOthersen_US
dc.description.fundingTextState Key Laboratory of Explosion Science and Technology, Beijing Institute of Technology; Natural Science Foundation of Chinaen_US
dc.description.pubStatusPublisheden_US
dc.identifier.OPUS25766276-
dc.description.oaCategoryGreen (AAM)en_US
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