Fatigue crack growth analysis of 2024 T3 aluminium specimens under aircraft service spectra
Methodology of a documentation assurance of industrial processes of a machine-building plant
New alloys for advanced metallic fighter-wing structures
Using microcomputers and specialized software to enhance aircraft design education
Farnborough international exhibition and flying display september 6th - 12th 1976
Reducing costs in aircraft: The metals affordability initiative consortium
Evaluation of a minimum principle for transonic flow computations by finite elements
Comparison of supercritical and conventional wing flutter characteristics
Nonlinear response of unidirectional and angle ply laminates