Why Not Run the Efficient Global Optimization Algorithm with Multiple Surrogates?
Using Response Surface Methodology in Fuzzy Set Based Design Optimization
Using Cross Validation to Design Conservative Surrogates
Using a Simple Crack Growth Model in Predicting Remaining Useful Life
University of Florida Micro Air Vehicle Competition Highlights
Uncertainty Reduction of Damage Growth Properties Using Structural Health Monitoring
Uncertainty in Wing Structural Weight Approximations
Uncertainty Identification of Damage Growth Parameters Using Nonlinear Regression (TN)
Uncertainty Analysis of Integrated Thermal Protection System with Rigid Insulation Bars
Two-Dimensional Orthotropic Plate Analysis for an Integral Thermal Protection System
Transport Weight Reduction through MDO: The Strut-Braced Wing Transonic Transport
TRANSPORTATION SAFETY AND THE ALLOCATION OF SAFETY IMPROVEMENTS
TRADE-OFFS OF WING WEIGHT AND LIFT/DRAG ON DESIGN OF MEDIUM-RANGE TRANSPORT AIRCRAFT
Tradeoffs of Wing Weight and Lift/Drag in Design of Medium-Range Transport Aircraft