Objectives/Expected Outcomes: To develop a specialist knowledge in the fields of computational, non-linear and unsteady aerodynamics. The develop familiarity with the techniques for predicting airflow/structure interactions for aerospace vehicles. Syllabus Summary: Advanced two and three dimensional panel method techniques; calculation of oscillatory flow results; prediction of aerodynamic derivatives. Pressure distributions for complete aircraft configuration. Unsteady subsonic flow analysis of aircraft; calculation of structural modes. Structural response to gusts; aeroelasticity; flutter and divergence. Solution of aerospace flow problems using finite element methods. Unsteady supersonic one-dimensional flow. Hypersonic flow; real gas effects. Introduction to the use of CFD for transonic flow.
Unit details and rules
Unit code | AERO5200 |
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Academic unit | Aerospace, Mechanical and Mechatronic |
Credit points | 6 |
Prohibitions
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None |
Prerequisites
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AERO9260 or AERO8260 or AERO3260 |
Corequisites
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None |
Assumed knowledge
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BE in the area of Aerospace Engineering or related Engineering field. |
Available to study abroad and exchange students | Yes |
Teaching staff
Coordinator | Gareth Vio, gareth.vio@sydney.edu.au |
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Lecturer(s) | Gareth Vio, gareth.vio@sydney.edu.au |