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=== Aviation engines ===
=== Aviation engines ===
*Hydraulic gas dynamics - characteristics of gas flowing through
*Hydraulic gas dynamics - characteristics of gas flowing through
*[[Theory of impeller machines]] - profiling blades of compressor and turbine, multistage compressor and multistage turbine
*[[Theory of impeler machines]] - profiling blades of compressor and turbine, multistage compressor and multistage turbine
*Theory of jet engines - modeling turbojet engines
*Theory of jet engines - modeling turbojet engines
*Construction of jet engines
*Construction of jet engines

Revision as of 16:15, 25 February 2008

For editors For lecturers For students

Welcome to the Department of Aerospace Engineering.

Aerospace Engineering deals specifically with aircraft and spacecraft, as well as any other types of machines that can fly. Topics within aerospace engineering include, but are not limited to, aerodynamics, structural dynamics, fluid mechanics, orbital mechanics, flight dynamics, propulsion, and control systems. These topics can be applied to missiles, space structures, satellites, and all aspects related to atmosphere and space flight.

Aerospace engineers design, develop, and test aircraft, spacecraft, and missiles and supervise the production of these products. Those who work with aircraft are called aeronautical engineers, and those working specifically with spacecraft are astronautical engineers. Aerospace engineers develop new technologies for use in aviation, defense systems, and space exploration, often specializing in areas such as structural design, guidance, navigation and control, instrumentation and communication, or production methods. They also may specialize in a particular type of aerospace product, such as commercial aircraft, military fighter jets, helicopters, spacecraft, or missiles and rockets, and may become experts in aerodynamics, thermodynamics, celestial mechanics, propulsion, acoustics, or guidance and control systems.

Areas of study

General Prerequisites

  • Basic Mathematics - differentials, integrals, basic mechanics, vector algebra, matrices and matrix manipulation, total derivative (for mass and momentum equations, among others)
  • Thermodynamics/Heat Transfer - Zereoth, First, Second and Third Laws, Enthalpy, Entropy, Clausius Inequality and ??, Steady State Equation, Modelling Gas Turbines/Engines, Conduction, Convection, Radiation (Black Body, Grey Body)
  • Circuits/Electronics
  • Physics - Forces, Gravity Equation

Statics

  • Structural Analysis
  • Mechanics - Friction on a surface, Rolling bodies, Stability, Pure/Damped/Forced Harmonic Motion, Orbits (reaching orbit, geostationary point, changing orbit, escape velocity)

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

Aircraft Structures

  • Basic Strength of Materials
  • Aircraft Structures - Basic
  • Aircraft Structures - Advanced
  • Structural Analysis
  • Recent Topics

Materials Science

Aircraft Design

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

Aviation engines

  • Hydraulic gas dynamics - characteristics of gas flowing through
  • Theory of impeler machines - profiling blades of compressor and turbine, multistage compressor and multistage turbine
  • Theory of jet engines - modeling turbojet engines
  • Construction of jet engines

Aeroelasticity

  • Introduction
  • Static Aeroelasticity
  • Dynamic Aeroelasticity
  • Flight Testing

Rover Design

Department news

The Aerospace Department is concerned with the technology that constitutes of Aeronautical and Astronautical engineering.

Books