1. Background to turbojet engines
The design and construction of a turbojet engine involves the use of materials (figure 1 ):
This is due to a wide operating temperature range, from -50 ˚C to 1,250 ˚C, and to the constant need to minimize mass;
working under severe mechanical and environmental conditions;
with long-lasting properties.
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Background to turbojet engines
Weldability standards specific to aerospace construction
Bibliography
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