Technical aspects:
Domain:
Airframe fuselage (metallic parts):
Frame,
Panel,
Stringer,
Cross Beam,
Frame coupling,
Skin doubler,
System brackets

Typical analysis to carry out:
o Strength analysis,
o Stabilities,
o Junctions (splicing, lug, panel junction ),
o Extract the loads and stress from global finite element model

Carry out the stress checking,
Examples of previous experience required in the domain:
Realize stress analyse from a clean sheet:
- Choose the correct methodologies to:
o Validate a particular area,
o Extract the loads and stresses from global finite element model,
o Realise local finite element models.

- Have experience in:
o Certification stress reports,
o Structural repair manual justification,
o Test correlation:
A/ C global test,

- Assist the design team by proposing:
o Design optimisations,
o Alternative solutions,

Modification of existing solutions:
o New system installation,
o Structural reinforcement,
o Weight optimisation,

An awareness of:
- Common design and manufacturing constrains,
- Fatigue and damage tolerance aspects.

Experience in the following would be appreciate:
- Composite aero structure,
- Fatigue and Damage tolerance analysis,
- Interiors,
- System installation