An integrated systems engineering approach to aircraft design
An integrated systems engineering approach to aircraft design
Dynamic Feedback Models for Whole Life Cost Prediction
AIAA-2003-6736 Research into Integrated Aircraft Technologies
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
Static Aeroelastic Effect of Local Skin Deformations on a NACA 0012 Airfoil
AIAA-2003-6747 Using Idealised Models to Enable Analysis Driven Design
AIAA-2006-7766 Value Driven Design Optimization of Aircraft Structures
AIAA-2006-7739 Integrating Design, Manufacturing and Cost for Trade-Offs on Aircraft Configurations
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Identifying Interfaces in Engineering Systems