Assignment for the TU Delft Master Course: AE4238 Aero Engine Technology
- The specific heat are assumed constant w.r.t. temperture
- Fuel does not alter the Individual gas constant of the exhaust air (hot nozzle)
- The intermediate values in a process can be approximated by an exponential function
- The flow through both nozzles is always choked
- Create config file for desired engine in accordance with the examples in
engine/data
- import the
Engine
class fromengine.py
and instantiate object w/ syntax:Engine(filename='myengine.cfg')
- Enjoy
Make table of governing relations between stages w/ assumptions