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