A Framework for Systematically Estimating Life Cycle Cost for an Integrated Wing
AIAA-2002-5852 Competitive Aircraft Design and Manufacture: The Next Frontier
AIAA-2003-6736 Research into Integrated Aircraft Technologies
AIAA-2003-6738 Methodologies and Issues Related to Technology Transfer Between Academia and Industry
AIAA-2003-6747 Using Idealised Models to Enable Analysis Driven Design
AIAA-2003-6827 Fabrication and Assembly Cost Drivers for Aircraft Manufacturing
AIAA-2003-6829 Aircraft Component Manufacture Case Studies and Operating Cost Reduction Benefit
AIAA-2004-6235 A Generic Tool for Cost Estimating in Aircraft Design
AIAA-2004-6457 Framework Tools for Modelling and Simulation Within an Integrated Design Environment
AIAA-2006-7739 Integrating Design, Manufacturing and Cost for Trade-Offs on Aircraft Configurations
AIAA-2006-7766 Value Driven Design Optimization of Aircraft Structures
Aircraft cost modelling using the genetic causal technique within a systems engineering approach
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Identifying Interfaces in Engineering Systems
An integrated systems engineering approach to aircraft design
An integrated systems engineering approach to aircraft design
Dynamic Feedback Models for Whole Life Cost Prediction
Impact of aerodynamic surface tolerance on aircraft cost driver
Impact of aerodynamic surface tolerance on aircraft cost driver
Life Cycle Cost Modeling for Aircraft Wing Using Object-Oriented Systems Engineering Approach
Static Aeroelastic Effect of Local Skin Deformations on a NACA 0012 Airfoil
Use of Digital Manufacturing to Improve Operator Learning in Aerospace Assembly