Paper Helicopter - Experimental Optimum Engineering Design Classroom Problem
Design of Shell Structures for Buckling Using Correction Response Surface Approximations
Topology Optimization of Transport Wing Internal Structure
Multifidelity Response Surface Model for HSCT Wing Bending Material Weight
Analysis and Design of Composite Curved Channel Frames
Response Surface Approximations for Structural Optimization
Analytical and Experimental Comparison of Probabilistic and Deterministic Optimization
HSCT Configuration Design Space Exploration Using Aerodynamic Response Surface Approximations
Construction of Response Surfaces for Design Optimization Applications