Aeroacoustic Assessment of Low-Observable UCAV Configurations
CIVIL PREPAREDNESS – NATO CIVIL EXPERTS CAPABILITY
Stability and Control CFD Investigations of a Generic 53 Degree Swept UCAV Configuration
Shock Tube and Ballistic Range Facilities at NASA Ames Research Center
Überblick Taktische Datenlinks
Vortex Flow Dilemmas and Control on Wing Planforms on High Speed
Comparison of X-31 Flight and Ground-Based Yawing Moment Asymmetries at High Angles of Attack
Joint Warrior Interoperability Demonstration (JWID) 2000
CNSC Meeting Held at NATO Headquarters, Brussels, from 9 to 11 October 2000
Multi-Objective Aeroelastic Optimization
Aspects of Aerodynamic Optimisation for Military Aircraft Design
Conceptual Design and Optimisation of Modern Combat Aircraft
Emergent Aerospace Designs Using Negotiating Autonomous Agents
Aerodynamics for MDO of an Innovative Configuration
General Keynote: Multi-Disciplinary Design of Combat Flight Vehicles