Synonyme wurden verwendet für:
optimization
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keywords:("optimization")
ADjoint: An Approach for Rapid Development of Discrete Adjoint Solvers
On the Common Structure of MDO Problems: A Comparison of Architectures
Three-Dimensional Structural Topology Optimization of an Aircraft Wing Using Level Set Methods
Toward High-Fidelity Aerostructural Optimization Using a Coupled ADjoint Approach
Aero-Structural Optimization of Non-Planar Lifting Surface Configurations
Aerostructural Optimization of Aircraft Structures Using Asymmetric Subspace Optimization
Progressive Validity Trust Region Optimization
Aerostructural Shape Optimization of Wind Turbine Blades Considering Site-Specific Winds
Multidisciplinary Design Optimization of Airframe and Engine for Emissions Reduction
A Configurable B-Spline Parametrization Method for Structural Optimization of Wing Boxes
Reconfigurable Semi-Analytic Sensitivity Methods and MDO Architectures within the piMDO Framework
A CAD-Free Approach to High-Fidelity Aerostructural Optimization
A New Approach to Multidisciplinary Design Optimization via Internal Decomposition
Stability-Constrained Aerodynamic Shape Optimization of a Flying Wing Configuration
A COMPARISON OF METALLIC AND COMPOSITE AIRCRAFT WINGS USING AEROSTRUCTURAL DESIGN OPTIMIZATION
GEOMACH: GEOMETRY-CENTRIC MDAO OF AIRCRAFT CONFIGURATIONS WITH HIGH FIDELITY
SIZING OF A SHORT RANGE CIVIL TRANSPORT AIRCRAFT CONSIDERING AERO-STRUCTURAL AND STABILITY EFFECTS
COUPLED OPTIMIZATION OF AIRCRAFT FAMILY DESIGN AND FLEET ASSIGNMENT FOR MINIMUM COST AND FUEL BURN
Aerodynamic Shape Optimization of an Adaptive Morphing Trailing Edge Wing
Strategies for Solving High-Fidelity Aerodynamic Shape Optimization Problems
Towards Gradient-Based Design Optimization of Flexible Transport Aircraft with Flutter Constraints
Geometry and Structural Modeling for High-Fidelity Aircraft Conceptual Design Optimization
Multidisciplinary Design Optimization of an Aircraft Wing Via a Matrix-Free Approach
Surrogate Models and Mixtures of Experts in Aerodynamic Performance Prediction for Mission Analysis
Aerostructural Optimization Of The Common Research Model Configuration