INIS
airplanes
16%
algorithms
16%
composite materials
16%
constraints
16%
design
100%
fibers
100%
guidelines
16%
increasing
33%
layers
33%
mechanical properties
33%
optimization
100%
stiffness
100%
thickness
100%
weight
33%
Engineering
Aircraft
16%
Composite
16%
Composite Material
16%
Curved Path
16%
Design Guideline
16%
Fiber
100%
Laminate
50%
Laminate Stiffness
100%
Laminate Thickness
100%
Limitations
16%
Mechanical Properties
33%
Obtains
16%
Optimised Design
33%
Optimization
16%
Optimization Approach
16%
Ply Angle
16%
Material Science
Composite Material
33%
Fiber
100%
Mechanical Strength
16%
Stiffness
100%