The aims of this module are to introduce the basic concepts of propulsion and to show how thrust and fuel consumption can be calculated for a variety of engines under design conditions. It will provide an understanding of the way in which materials constraints and aerodynamics limit gas-turbine and aero-engine performance, particularly of turbines and compressors and will introduce the basic principles of turbine, compressor and nozzle design

Sorry, there are no lists here yet. You could try:

  • Clicking My Lists from the menu. Your course enrolled lists are stored here.
  • Searching for the list using the form below:

Lists linked to Aircraft Propulsion

There are currently no lists linked to this Module.