A technique of computer-aided synthesizing a finite element model of wing center section and outer wing torsion box joint for a transport aircraft
Russian aeronautics ; 57 , 1
2014
Article (Journal)
English
BKL: | 55.50 Luftfahrzeugtechnik | |
Local classification TIB: | 770/7040/8000 |
JOINT BETWEEN AIRCRAFT CENTRE WING SECTION AND OUTER WING
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