I was just about to start a new thread with a question that has interested me for some time, when I thought I had better do a search first
So this seems to be the perfect place to ask my question.
In a turbojet, which parts of the engine does the thrust reaction force act on and in roughly what percentage?
To put it another way, which parts of the engine transfer the thrust reaction force to the engine mountings and thence to the airframe?