Keyphrases
Multidisciplinary Design Optimization
99%
Aircraft Design
87%
Shape Optimization
82%
Design Process
78%
Structural Optimization
69%
Airframe Design
56%
Design Space
54%
Detailed Sizing
45%
Design Optimization
39%
Stacking Sequence
39%
Form-finding
36%
Parametrization
36%
Composite Simpson Rule
36%
Aeroelastic Loads
36%
Stacking Sequence Optimization
36%
High Performance
36%
Aerial Vehicle
36%
Process Optimization
36%
Gradient-based Optimization
33%
Conceptual Design Phase
33%
Composite Laminates
30%
Kinematics
27%
Aircraft Development
27%
Fiber Reinforced Polymer
27%
Aircraft Wing
27%
Mesoscale Models
27%
Sizing Optimization
24%
Two-stage Approach
24%
Discrete Design
24%
Mixed Integer Linear Programming Formulation
24%
Military Aircraft
24%
Aerostructures
23%
Failure Criterion
22%
Filter Method
22%
Aero-structural
22%
Composite Structures
21%
Structural Sizing
21%
Design Requirements
19%
Early Design Phases
19%
Anisotropic Stress Field
18%
Post-buckling Behavior
18%
Composite Aircraft Structures
18%
Collaborative Product Development
18%
Physical Experiment
18%
Thin-walled Shell
18%
Blending Optimization
18%
Discrete Adjoint Sensitivities
18%
Parameterized Geometry
18%
Area Current
18%
Laminated Structure
18%
Engineering
Design Process
100%
Multidisciplinary Design Optimization
99%
Airframe
62%
Regularization
54%
Design Space
54%
Parametrization
54%
Design Optimization
54%
Development Process
46%
Form Finding
45%
Computer Aided Design
42%
Preliminary Design
40%
Objective Function
36%
Filtration
36%
Military Aircraft
36%
Engineering
33%
Composite Material
33%
Composite Structure
30%
Design Phase
28%
Finite Element Analysis
28%
Wings
27%
Mesh Distortion
27%
Mixed-Integer Linear Programming
27%
Flight Condition
27%
Mesoscale
27%
Fiber-Reinforced Polymer
27%
Conceptual Design Phase
24%
Optimal Design
21%
Stress State
21%
Failure Criterion
19%
Aerodynamics
19%
Stiffness Property
18%
Aircraft
18%
Aircraft Structure
18%
Performance Aircraft
18%
Innovative Development
18%
Composite Aircraft Structure
18%
Fine Mesh
18%
Laminated Structure
18%
Anisotropic
18%
Air System
18%
Development Cycle
18%
Model Geometry
18%
Illustrates
18%
Numerical Methods
18%
Gust Loads
18%
Computational Expense
18%
Damage Model
18%
Simulation Mode
18%
Development Phase
18%
Aerospace Material
18%
