Contents of Some Previous Issues - Volume 34 - Erratum - Impulse noise and its control
Aerodynamic performance of contra-rotating Wells turbine for wave energy conversion
Impact of aerodynamic surface tolerance on aircraft cost driver
Impact of aerodynamic surface tolerance on aircraft cost driver
AIAA-2003-6738 Methodologies and Issues Related to Technology Transfer Between Academia and Industry
Computational Study of Passive Boundary Layer Control Applied to a Supersonic Intake
Aerodynamic performance of a bypass engine with fan nozzle exit area change by warped chevrons
A Study of Isolated Nacelle Flows at Subsonic and Transonic Speeds
Dynamic Feedback Models for Whole Life Cost Prediction
Systems Engineering for CDIO - Conceive, Design, Implement and Operate AIAA Paper
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-2004-6340 A Computational Investigation of Propulsion Integration
Performance and Acoustic Optimisation of Nacelle Nozzle Throat Area
A Framework for Systematically Estimating Life Cycle Cost for an Integrated Wing
Aerodynamic Performance of Modified NACA Profiles for Wells Turbine Applications
Effect of Heat Transfer on Transonic Flow over an Airfoil
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
ICAS-92-3.3.4 Passive Boundary-Layer Bleed for Supersonic Intakes
Static Aeroelastic Effect of Local Skin Deformations on a NACA 0012 Airfoil