3 ms·
is point 1 typical for all turbojet & turbofan engines, or is this specific to then J58?
by yock 14y ago
is point 1 typical for all turbojet & turbofan engines, or is this specific to then J58?
- tcas 14y agoOn modern jet engines: yes. There's a documentary / video about the manufacture of the Rolls-Royce Trent engine that mentions this fact and shows a CAD drawing / part of the manufacture process of the blades right after the combustion stage.