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