Engineering
Composite
100%
Stiffened Panel
100%
Aircraft Structure
100%
Progressive Failure
50%
Analysis Method
50%
Obtains
50%
Fuselage Skin
50%
Aircraft
50%
Skin Panel
50%
Final Design
50%
Failure (Mechanical)
50%
Gas Fuel Manufacture
50%
Failure Model
50%
Test Result
50%
Resin Transfer Molding
50%
Fabrication Method
50%
INIS
design
100%
testing
100%
fabrication
100%
grids
100%
aircraft
100%
panels
100%
prediction
28%
failures
28%
finite element method
28%
damage
28%
skin
28%
molding
14%
production
14%
compression
14%
manufacturing
14%
tolerance
14%
weight
14%
resins
14%
cost
14%
passengers
14%
iterative methods
14%
Material Science
Composite Material
100%
Aircraft
100%
Finite Element Modeling
100%
Sandwich Panel
50%
Damage Tolerance
50%
Resin Transfer Molding
50%
Residual Strength
50%