AIAA-2003-6747 Using Idealised Models to Enable Analysis Driven Design
Challenges in Collaborative Simulation for the Virtual Enterprise
Enhancement of thrust reverser cascade performance using aerodynamic and structural integration
Influence of flight control laws on structural sizing of commercial aircraft
Integrated Methods for the Design of a Thrust Reverser Cascade
Load Case Characterization for the Aircraft Structural Design Process
Load Case Characterization for the Aircraft Structural Design Process
Modular Mission Payloads Plug and Play Demonstration
Oregon Forestry: In A State of Change, Examining Social Forest Assessments