REPRESENTATION OF STRUCTURAL SOLUTIONS IN BLENDED WING BODY PRELIMINARY DESIGN
A Method for the Assessment of Ageing Properties of Structural Lightweight Components
1.B.2 Feasibility Study of the Application of GLARE Materials in Wide Body Aircraft Fuselages
Stability Estimation for Stiffened Structures Considering Laser Beam Welded Stringers
Extensions to Aircraft Pre-design for Supersonic Aircraft (AIAA 2014-0184)
Lessons Learned from Recent European Research Projects on Ageing Aircraft
Numerical `Round Robin' Tests on the Assessment of MSD
IC-126 Material forces as a novel criterion for crack-turning in stiffened structures
Preliminary Design of a Blended Wing Body Configuration using the Design Tool PrADO
Preliminary Design of a Blended Wing Body Configuration using the Design Tool PrADO