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Why Not Run the Efficient Global Optimization Algorithm with Multiple Surrogates?
Reliability-Based Structural Design of Aircraft Together with Future Tests
Homogenization of Integrated Thermal Protection System with Rigid Insulation Bars
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
Effective Tests for Discovering Unexpected Structural Failure Modes
Estimating Probability of Failure of Composite Laminated Panel with Multiple Failure Modes
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
Surrogate-Based Agents for Constrained Optimization
Accounting for Future Redesign in the Optimization of an Integrated Thermal Protection System
Efficient Global Optimization with Adaptive Target for Probability of Targeted Improvement
Uncertainty Analysis of Integrated Thermal Protection System with Rigid Insulation Bars
Contribution of Building-block Test to Discover Unexpected Failure Modes
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
Probability of Failure Uncertainty Quantification with Kriging
Synchronizing Condition-based Maintenance with Necessary Scheduled Maintenance
Statistical Characterization of Damage Propagation Properties in Structural Health Monitoring
Importing Uncertainty Estimates from One Surrogate to Another
Improving Diagnosis from Past Prognosis in Structural Health Monitoring
Options for Using Test Data to Update Failure Stress AIAA Paper 2007-1971 CD-ROM Number 8
Multi-Fidelity Design of an Integrated Thermal Protection System for Spacecraft Reentry
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
Sensitivity of Stress Constraints Using the Adjoint Method
Using Response Surface Methodology in Fuzzy Set Based Design Optimization
AIAA-2001-1205 Composite Wing Structural Design Optimization with Continuity Constraints
Permutation Genetic Algorithm for Stacking Sequence Optimization
AIAA-2001-1680 Uncertainty and Response Surface Approximations