Laserbasierte Messtechnik optimiert Flugzeugfertigung
Evaluation of a minimum principle for transonic flow computations by finite elements
Multilevel framework for optimization of lightweight structures
New alloys for advanced metallic fighter-wing structures
Comparison of supercritical and conventional wing flutter characteristics
Nonlinear response of unidirectional and angle ply laminates
Numerical optimization of a composite high lift structure
Using microcomputers and specialized software to enhance aircraft design education
Farnborough international exhibition and flying display september 6th - 12th 1976
Structural optimization of composite aircraft panels with large cut-outs
Reducing costs in aircraft: The metals affordability initiative consortium