Please use this identifier to cite or link to this item: https://repository.sustech.edu/handle/123456789/3091
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dc.contributor.authorAli, Esra Abd Alhleem Hassan-
dc.date.accessioned2014-01-09T10:10:27Z-
dc.date.available2014-01-09T10:10:27Z-
dc.date.issued2010-01-01-
dc.identifier.citationAli,Esra Abd Alhleem Hassan.A STUDY SUBSONIC AND HYPERSONIC FLOW ON AN AIRFOIL/Esra Abd Alhleem Hassan Ali;Osman Mohamed El-Mekki.-Khartoum:Sudan University of Science and Technology,College of Science,2010.-41p. : ill. ; 28cm.-M.Sc.en_US
dc.identifier.urihttp://hdl.handle.net/123456789/3091-
dc.descriptionThesisen_US
dc.description.abstractFirst in this research I study's about (subsonic and hypersonic flows on an airfoil)which consists of three Chapters; Chapter one by the title: (Compressible Potential Flow)contains: Introduction, Speed of sound, Irrotational flow, :Linearized potential equation which includes Applications, Perturbation potentials), Pressure ) coefficient of small perturbations, Relation for subsonic compressible flow including (Airfoils (2-D flow), Boundary conditions, Pressure coefficients), .Critical Mach numberandSupercritical airfoils However, in Chapter two (Two-Dimential subsonic and supersonic equation) solution which of the includes: linearized Effects of .compressibility, Linearized theory In the Chapter threewith the title: (Small Disturbance Theory) includes: Centered Prandtel- Meyer rereflction,Wave Interactions, including: (Oblique shock reflected from a wall, Oblique shock intersection), Shock strengthening, .Supersonic flow over airfoilsen_US
dc.description.sponsorshipSudan University of Science and Technologyen_US
dc.language.isoenen_US
dc.publisherSudan University of Science and Technologyen_US
dc.subjectMathematicsen_US
dc.subjectDimential subsonicen_US
dc.subjectSupersonicen_US
dc.subjectHypersonicen_US
dc.titleA STUDY SUBSONIC AND HYPERSONIC FLOW ON AN AIRFOILen_US
dc.typeThesisen_US
Appears in Collections:Masters Dissertations : Science

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