Zobrazeno 1 - 1
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pro vyhledávání: '"Damodar R. Anbur"'
Publikováno v:
Journal of Aircraft. 32:1382-1389
A combined loads test machine used to test aircraft primary structures such as fuselage and wing sections is described. The design features of a D-box test fixture that provides a simple test setup with the flexibility to accommodate curved stiffened