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Coupled Fluid–Structural Thermal Numerical Methods for Thermal Protection System

2019; American Institute of Aeronautics and Astronautics; Volume: 57; Issue: 8 Linguagem: Inglês

10.2514/1.j057616

1533-385X

Jie Huang, Weixing Yao, Xian-Yang Shan, Cheng Chang,

Rocket and propulsion systems research

No AccessTechnical NotesCoupled Fluid–Structural Thermal Numerical Methods for Thermal Protection SystemJie Huang, Wei-Xing Yao, Xian-Yang Shan and Cheng ChangJie HuangState Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People's Republic of China, Wei-Xing YaoState Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People's Republic of China, Xian-Yang ShanHubei Aerospace Technology Academy, 430040 Wuhan, People's Republic of China and Cheng ChangState Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People's Republic of ChinaPublished Online:24 Jun 2019https://doi.org/10.2514/1.J057616SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Yadav R. and Guven U., "Aerodynamic Heating of a Hypersonic Projectile with Forward-Facing Ellipsoid Cavity at Nose," Journal of Spacecraft and Rockets, Vol. 52, No. 1, 2015, pp. 157–165. doi:https://doi.org/10.2514/1.A32605 LinkGoogle Scholar[2] Huang J., Yao W. 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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. TopicsAerothermodynamicsComputational Fluid DynamicsFinite Element MethodFinite Element SoftwareFinite Volume MethodFluid DynamicsHeat ConductionHeat FluxHeat TransferThermal Control and ProtectionThermodynamic PropertiesThermodynamicsThermophysical PropertiesThermophysics and Heat Transfer KeywordsThermal Protection SystemCFD AnalysisTemperature FieldsAerodynamic HeatingThermal ConductivityNumerical AnalysisReynolds Averaged Navier StokesStructural Heat Transfer AnalysisMach NumberWall TemperatureAcknowledgmentThis research was supported by the Priority Academic Program Development of Jiangsu Higher Education Institutions and National Postdoctoral Program for Innovative Talents.PDF Received12 June 2018Accepted21 April 2019Published online24 June 2019