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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
A Multilevel Wing Design Procedure Centered on the ASTROS Structural Optimization System
Modeling and Simulation of Airworthiness Requirements for an HSCT Prototype in Early Design
Robust Design for Aeroelastically Tailored/Active Aeroelastic Wing
Multi-Level, Partitioned Response Surfaces for Modeling Complex Systems
Conceptual Aircraft Design Environment: Case Study Evaluation of Computing Architecture Technologies
A Generic Mathematical Model of Groundroll Motion of a High Speed Transport Airplane
AIAA-2002-5411 Optimizing the Parallel Process Flow for the Individual Discipline Feasible Method
AIAA-2002-5424 Technology Portfolio Assessments Using a Modified Genetic Algorithm Approach
AIAA-2002-5603 Robust Structural Design of an Active Aeroelastic Wing with Maneuver Load Uncertainty
AIAA-2002-5426 A Bi-level Optimization Approach for Technology Selection
AIAA-2002-5620 System of Systems Modeling for Personal Air Vehicles
AIAA-2002-5423 A Multi-Level, Hierarchical Approach to Technology Selection and Optimization