Multi-Level, Partitioned Response Surfaces for Modeling Complex Systems
A Generic Mathematical Model of Groundroll Motion of a High Speed Transport Airplane
Modeling and Simulation of Airworthiness Requirements for an HSCT Prototype in Early Design
Conceptual Aircraft Design Environment: Case Study Evaluation of Computing Architecture Technologies
Robust Design for Aeroelastically Tailored/Active Aeroelastic Wing
A Multilevel Wing Design Procedure Centered on the ASTROS Structural Optimization System
Integrated Product Development for the Wing Structural Design of the High Speed Civil Transport
Application of a Concurrent Engineering Methodology to the Design of a Dual Use VTOL Aircraft