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• W2919009862 abstract "No AccessTechnical NotesNumerical Experiments on Anomalies from Stationary, Slowly Moving, and Fast-Moving ShocksKeiichi Kitamura and Eiji ShimaKeiichi KitamuraYokohama National University, Yokohama 240-8501, Japan*Associate Professor, School of Engineering, 79-5 Tokiwadai, Hodogaya-ku. Senior Member AIAA.Search for more papers by this author and Eiji ShimaJapan Aerospace Exploration Agency, Sagamihara, Kanagawa 252-5210, Japan†Research and Development Directorate, Research Unit III (JAXA’s Engineering Digital Innovation Center), 3-1-1 Yoshinodai, Chuo. Senior Member AIAA.Search for more papers by this authorPublished Online:4 Mar 2019https://doi.org/10.2514/1.J057366SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Quirk J. 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Google Scholar Previous article Next article FiguresReferencesRelatedDetailsCited byOn Peculiar Behaviors of Captured Very-Weak Moving ShockwavesGaku Fukushima, Keiichi Kitamura and Akihiro Sasoh20 June 2022A Review of Riemann Solvers for Hypersonic Flows21 October 2021 | Archives of Computational Methods in Engineering, Vol. 29, No. 3Space-time mesh refinement method for simulating transient mixed flows11 January 2021 | Journal of Hydraulic Research, Vol. 59, No. 5Suppress Numerical Oscillations in Transient Mixed Flow Simulations with a Modified HLL Solver27 April 2020 | Water, Vol. 12, No. 5Role and History of Numerical Flux Functions1 November 2020 What's Popular Volume 57, Number 4April 2019 CrossmarkInformationCopyright © 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 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAerodynamicsAeronautical EngineeringAeronauticsComputational Fluid DynamicsEquations of Fluid DynamicsFinite Volume MethodFlow RegimesFluid DynamicsNormal Shock WaveNumerical AnalysisShock Waves KeywordsHugoniot CurveBlunt BodiesRankine Hugoniot RelationCourant Friedrichs LewyFVMSpecific HeatHigh Aspect RatioHypersonic FlowsTotal EnergyNormal Shock WaveAcknowledgmentsThis work was partially conducted while Keiichi Kitamura was under supervision of Eiji Shima at the Japan Aerospace Exploration Agency, supported by the Japan Society for the Promotion of Science. Tsutomu Saito, Muroran Institute of Technology, Japan, gave the authors a helpful comment. The authors thank their cooperation.PDF Received1 April 2018Accepted17 January 2019Published online4 March 2019" @default.
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