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Werkstoff
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Estimating Probability of Failure of Composite Laminated Panel with Multiple Failure Modes
Surrogate-Based Agents for Constrained Optimization
Accounting for Future Redesign in the Optimization of an Integrated Thermal Protection System
Effective Tests for Discovering Unexpected Structural Failure Modes
Efficient Global Optimization with Adaptive Target for Probability of Targeted Improvement
Probability of Failure Uncertainty Quantification with Kriging
Synchronizing Condition-based Maintenance with Necessary Scheduled Maintenance
Contribution of Building-block Test to Discover Unexpected Failure Modes
Uncertainty Analysis of Integrated Thermal Protection System with Rigid Insulation Bars
Efficient Global Optimization with Experimental Data: Revisiting the Paper Helicopter Design
Structural and Aeroelastic Characteristics of Truss Braced Wings: A Parametric Study
Effect of Inspection Strategies on the Weight and Lifecycle Cost of Airplanes
Improving Diagnosis from Past Prognosis in Structural Health Monitoring
Including Future Tests in the Design and Optimization of an Integrated Thermal Protection System
Design Optimization of a Bendable UAV Wing Under Uncertainty
Homogenization of Plates with Microstructure and Application to Corrugated Core Sandwich Panels
Homogenization of Integrated Thermal Protection System with Rigid Insulation Bars
Why Not Run the Efficient Global Optimization Algorithm with Multiple Surrogates?
Reliability-Based Structural Design of Aircraft Together with Future Tests
Effects of Structural Tests on Aircraft Safety
Conservative Reliability Estimates in Design Optimization Using Multiple Tail Median
Multi-Fidelity Analysis of Corrugated-Core Sandwich Panels for Integrated Thermal Protection Systems
Statistical Characterization of Damage Propagation Properties in Structural Health Monitoring
Importing Uncertainty Estimates from One Surrogate to Another
Options for Using Test Data to Update Failure Stress AIAA Paper 2007-1971 CD-ROM Number 8
AIAA-2006-2059 Reliability Based Aircraft Structural Design Pays Even with Limited Statistical Data
AIAA-2006-1632 Taking Advantage of Separable Limit States in Sampling Procedures
AIAA-2004-1670 Safety Factor and Inverse Reliability Measures
AIAA-2004-1910 A Double-Distribution Statistical Algorithm for Composite Laminate Optimization
AIAA-2004-1541 Decomposition and Two-level Optimization of Structures with Discrete Sizing Variables
Tradeoffs of Weight and Inspection Cost in Fail-safe Design
Optimization Design of Composite Plates with Holes for Increased Strength
Arresting Cracks in Bone-like Composites
Reliability-based Design Optimization Using Probabilistic Safety Factor
Piezoresistive Microphone Design Pareto Optimization: Tradeoff Between Sensitivity and Noise Floor
Effect of Compressive Force on Flutter Speed of a Strut-Braced Wing
Minimum Mass Design of Insulation Made of Functionally Graded Material
Optimization Design of Inhomogeneous Isotropic Plates with Holes by Mimicking Bones