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Aeroelastic Modelling and Design of Aeroelastically Tailored and Morphing Wings
Noud Werter
Aerospace Structures & Computational Mechanics
Research output
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Thesis
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Dissertation (TU Delft)
547
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INIS
design
100%
modeling
100%
optimization
42%
aircraft
42%
efficiency
28%
performance
28%
control
14%
dynamics
14%
composite materials
14%
air
14%
deformation
14%
range
14%
shape
14%
space
14%
growth
14%
nasa
14%
environment
14%
stiffness
14%
Engineering
Design
100%
Wings
100%
Optimization
30%
Operational Efficiency
20%
Aeroelastic Tailoring
20%
Models
10%
Stiffness Property
10%
Aircraft
10%
Composite Material
10%
Cruise Condition
10%
NASA
10%
Directional
10%
Illustrates
10%
Design Space
10%
Unmanned Aerial Vehicle
10%