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* Basic Aircraft Performance - Air density at altitudes, Perfect Gas equation,
* Basic Aircraft Performance - Air density at altitudes, Perfect Gas equation,
* Dynamics and Control - Control Surfaces,
* Dynamics and Control - Control Surfaces,
[[Category:Aerospace Engineering|!]]
[[Category:Engineering]]

Revision as of 00:32, 21 November 2006

Aerospace Engineering

For editors For lecturers For students

Suggested Structure

General Prerequisites

Statics

Fluid mechanics

  • Aerodynamics - Derivation of shear stress on a fluid, perfect gas equation, Bernoulli equation, Langrangian and Eulerian reference frames, control volumes and control surfaces, Conservation of mass up to 3-d, balance of momentum equations up to 3-d, Aerofoils, Circulation, Mach Number & Renauld's Number, Laminar and turbulent flow
  • Propulsion - Turbomachinery

Materials Science

  • Material Classes - Metals, Ceramics, Composites, Polymers, Ionic and Covalents
  • Material Microstructure
  • Properties of Materials - Strength, Stiffness, Young's Modulus, Elasiticity and Modulus of Elasticity, Hardness, Toughness, Electrical Properties?
  • Materials Selection
  • Material Processes - Annealing, Quenching, Precipitaiton Hardening, Case Hardening
  • Failure - Fatigue, Creep, Fracture, Case studies (aircraft)
  • Composites - matrix and fibers, explanation of directional properties, case studes (carbon fibre, kevlar, fibreglass)

Aircraft Design

  • Basic Aircraft Performance - Air density at altitudes, Perfect Gas equation,
  • Dynamics and Control - Control Surfaces,