In this chapter, the operation of a basic turbojet engine is described. This is followed by a discussion of the individual components, namely, the compressor, combustor, turbine and the nozzle. This discussion brings out the details of the operation of these components along with important issues related to their operation. A thermodynamic analysis of the operation of the whole engine as well as the components is deferred till Chap. 7.
The Turbojet Engine
Fundamentals of Propulsion ; Chapter : 5 ; 61-81
2021-08-26
21 pages
Article/Chapter (Book)
Electronic Resource
English
Online Contents | 1996
Engineering Index Backfile | 1952
Engineering Index Backfile | 1952