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Effective Technique to Improve Shock Anomalies and Heating Prediction for Hypersonic Flows

2017; American Institute of Aeronautics and Astronautics; Volume: 55; Issue: 4 Linguagem: Inglês

10.2514/1.j055347

1533-385X

Zhenhua Jiang, Chao Yan, Jian Yu, Bo Gao,

Fluid Dynamics and Turbulent Flows

No AccessTechnical NoteEffective Technique to Improve Shock Anomalies and Heating Prediction for Hypersonic FlowsZhen-Hua Jiang, Chao Yan, Jian Yu and Bo GaoZhen-Hua JiangBeijing University of Aeronautics and Astronautics, 100191 Beijing, People's Republic of China, Chao YanBeijing University of Aeronautics and Astronautics, 100191 Beijing, People's Republic of China, Jian YuBeijing University of Aeronautics and Astronautics, 100191 Beijing, People's Republic of China and Bo GaoBeijing Institute of Astronautics System Engineering, 100076 Beijing, People's Republic of ChinaPublished Online:28 Feb 2017https://doi.org/10.2514/1.J055347SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Kitamura K., Roe P. and Ismail F., "Evaluation of Euler Fluxes for Hypersonic Flow Computations," AIAA Journal, Vol. 47, No. 1, 2009, pp. 44–53. doi:https://doi.org/10.2514/1.33735 LinkGoogle Scholar[2] Kitamura K., Shima E., Nakamura Y. and Roe P., "Evaluation of Euler Fluxes for Hypersonic Heating Computations," AIAA Journal, Vol. 48, No. 4, 2010, pp. 763–776. doi:https://doi.org/10.2514/1.41605 LinkGoogle Scholar[3] Kitamura K., Shima E. and Roe P., "Carbuncle Phenomena and Other Shock Anomalies in Three Dimensions," AIAA Journal, Vol. 50, No. 12, 2012, pp. 2655–2669. doi:https://doi.org/10.2514/1.J051227 LinkGoogle Scholar[4] Kitamura K., "Assessment of SLAU2 and Other Flux Functions with Slope Limiters in Hypersonic Shock-Interaction Heating," Computers and Fluids, Vol. 129, April 2016, pp. 134–145. doi:https://doi.org/10.1016/j.compfluid.2016.02.006 CrossrefGoogle Scholar[5] Tu G., Zhao X., Mao M., Chen J., Deng X. and Liu H., "Evaluation of Euler Fluxes by a High-Order CFD Scheme: Shock Instability," International Journal of Computational Fluid Dynamics, Vol. 28, No. 5, 2014, pp. 171–186. doi:https://doi.org/10.1080/10618562.2014.911847 CrossrefGoogle Scholar[6] Muller B., "Simple Improvements of an Upwind TVD Scheme for Hypersonic Flow," AIAA Paper 1989-1977, 1989. LinkGoogle Scholar[7] Nicols R. H., Tramel R. W. and Bunning P. G., "Evaluation of Two High-Order Weighted Essentially Nonoscillatory Schemes," AIAA Journal, Vol. 46, No. 12, 2008, pp. 3090–3102. doi:https://doi.org/10.2514/1.36849 LinkGoogle Scholar[8] Yu J. and Yan C., "On the Performance of Two Shock-Capturing Schemes," Journal of Beijing University of Aeronautics and Astronautics, Vol. 36, No. 1, 2010, pp. 10–13. Google Scholar[9] Rider W. J., "Methods for Extending High-Resolution Schemes to Non-Linear Systems of Hyperbolic Conservation Laws," International Journal for Numerical Methods in Fluids, Vol. 17, No. 10, 1993, pp. 861–885. doi:https://doi.org/10.1002/fld.1650171004 CrossrefGoogle Scholar[10] Gnoffo P. A., "Multi-Dimensional, Inviscid Flux Reconstruction for Simulation of Hypersonic Heating on Tetrahedral Grids," AIAA Paper 2009-0599, 2009. LinkGoogle Scholar Previous article Next article FiguresReferencesRelatedDetailsCited byNumerical study of reverse jet for mitigating shock/shock interaction heatingAerospace Science and Technology, Vol. 131Passive Flow Control for Heat Flux Reduction on V-Shaped Blunt Leading EdgesOn the use of thermally perfect gas model for heating prediction of laminar and turbulent SWBLIAerospace Science and Technology, Vol. 95A new formulation for two-wave Riemann solver accurate at contact interfacesPhysics of Fluids, Vol. 31, No. 4A combined criteria-based method for hypersonic three-dimensional boundary layer transition predictionAerospace Science and Technology, Vol. 73 What's Popular Volume 55, Number 4April 2017 CrossmarkInformationCopyright © 2016 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 ISSN 0001-1452 (print) or 1533-385X (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAerodynamicsAeronautical EngineeringAeronauticsAerospace SciencesComputational Fluid DynamicsConservation of Momentum EquationsEquations of Fluid DynamicsFlow RegimesFluid DynamicsNumerical AnalysisShock Waves KeywordsHypersonic FlowsFreestream Mach NumberPrimitive VariableNumerical ModelingUpwind SchemeHypersonic ShockComputingNavier Stokes EquationsWall TemperatureNonlinear SystemsAcknowledgmentThe research is supported by the National Natural Science Foundation of China (11372054).PDF Received9 May 2016Accepted26 November 2016Published online28 February 2017