Skip to main content

We are aiming for an incremental return to campus in accordance with guidelines provided by NSW Health and the Australian Government. Until this time, learning activities and assessments will be planned and scheduled for online delivery where possible, and unit-specific details about face-to-face teaching will be provided on Canvas as the opportunities for face-to-face learning become clear.

Unit of study_

AERO5200: Advanced Aerodynamics

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.

Code AERO5200
Academic unit Aerospace, Mechanical and Mechatronic
Credit points 6
Prerequisites:
? 
AERO9260 or AERO8260 or AERO3260
Corequisites:
? 
None
Prohibitions:
? 
None
Assumed knowledge:
? 
BE in the area of Aerospace Engineering or related Engineering field.

At the completion of this unit, you should be able to:

  • LO1. understand the limitations of theory and the effect of second-order parameters (Reynolds number, Mach Number) to the primary fluid-flow properties
  • LO2. construct simple computer algorithms that will allow more complex geometries to be solved and determine the best approach from survey of existing methods
  • LO3. predict flow properties for general aircraft wing sections to obtain lift, drag and pitching moment
  • LO4. extrapolate section results to predict unsteady flow effects and three-dimensional wing behaviour
  • LO5. demonstrate an improved understanding of the use of software packages to solve fluid flow problems
  • LO6. undertake experiments and analyse data to verify theoretical predictions.

Unit outlines

Unit outlines will be available 2 weeks before the first day of teaching for 1000-level and 5000-level units, or one week before the first day of teaching for all other units.

There are no unit outlines available online for previous years.