Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/18926
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dc.contributor.authorPhua, Xi Kun.-
dc.date.accessioned2009-08-18T04:00:17Z-
dc.date.available2009-08-18T04:00:17Z-
dc.date.copyright2009en_US
dc.date.issued2009-
dc.identifier.urihttp://hdl.handle.net/10356/18926-
dc.description.abstractThe purpose of this paper is to explore the development of a numerical scheme which employs a more general Riemann Problem (generalized Riemann Problem, or GRP). A key characteristic of this GRP is the use of higher-order functions (instead of first-order piecewise functions) for approximating the actual flow, so as to obtain a more accurate numerical solution. The key motivation behind the development of GRP is to ultimately apply to aerodynamic applications. However, for testing purposes, it is more convenient to validate the GRP on a simpler flow scenario (governed by the same physical laws as most aerodynamic flows of numerical concern). Our test case would be the shock tube problem.en_US
dc.format.extent71 p.en_US
dc.language.isoenen_US
dc.rightsNanyang Technological University-
dc.subjectDRNTU::Engineering::Aeronautical engineering::Aerodynamicsen_US
dc.titleDevelopment of a generalized Riemann problem for aerodynamic applicationsen_US
dc.typeFinal Year Project (FYP)en_US
dc.contributor.supervisorRoxana Vasilescuen_US
dc.contributor.schoolSchool of Mechanical and Aerospace Engineeringen_US
dc.description.degreeBachelor of Engineering (Aerospace Engineering)en_US
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Appears in Collections:MAE Student Reports (FYP/IA/PA/PI)
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