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Including Future Tests in the Design and Optimization of an Integrated Thermal Protection System
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
Efficient Global Optimization with Adaptive Target for Probability of Targeted Improvement
Design Optimization of a Bendable UAV Wing Under Uncertainty
Homogenization of Plates with Microstructure and Application to Corrugated Core Sandwich Panels
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
Conservative Reliability Estimates in Design Optimization Using Multiple Tail Median
Multi-Fidelity Analysis of Corrugated-Core Sandwich Panels for Integrated Thermal Protection Systems
Probability of Failure Uncertainty Quantification with Kriging
Synchronizing Condition-based Maintenance with Necessary Scheduled Maintenance
Effect of Inspection Strategies on the Weight and Lifecycle Cost of Airplanes
Statistical Characterization of Damage Propagation Properties in Structural Health Monitoring
Importing Uncertainty Estimates from One Surrogate to Another
Effects of Structural Tests on Aircraft Safety
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
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
Using Response Surface Methodology in Fuzzy Set Based Design Optimization
Sensitivity of Stress Constraints Using the Adjoint Method
A Two Species Genetic Algorithm for Designing Composite Laminates Subjected to Uncertainty
AIAA-2001-1680 Uncertainty and Response Surface Approximations
AIAA-2001-1205 Composite Wing Structural Design Optimization with Continuity Constraints