Simultaneous Dynamic and corrosive Test, a Real World test Method for Aircraft Structure Components

摘要

Today the structures of civil and military aircrafts mostly are assembled of sheets of high strength aluminum alloys which are fastened to the internal structure. These joints cause considerable problems because they are exposed to corrosive and dynamic load. Especially this is the case when sheets and fasteners are man- ufactured of high strength material. One example are sheets of the alloy AA2024 T351 with fasteners of the titanium alloy Ti6Al 4V.