Theory of Aerospace Propulsion 2 |
NAKAJIMA, Takashi |
| Elective Requisites 2 credits |
|
【Aerospace Engineering･2nd semester】
16-1-0290-2641 |
| １． |
Objectives |
|
In these days, aeroplanes have applied several types of gas-turbine engines to their propulsion system such as the Turbojet engine, Turbofan engine, Turbo-prop engine, Turbo-shaft engine etc..
In this course, students will master general knowledge about aero-turbo engines and learn to understand the characteristics and roles of each.
|
| ２． |
Outline |
|
The configuration, function and performance of the aero-turbo engine will be studied based on the basic knowledge of thermodynamics and/or fluid-dynamics.
|
|