Destructive examinations were performed to document the progression of multi-site damage (MSD) in three lap joint panels that were removed from a full scale fuselage test article that was tested to 60,000 full pressurization cycles. Similar fatigue crack growth characteristics were observed for small cracks (50 microns to 10 mm) emanating from counter bore rivets, straight shank rivets, and 100 deg counter sink rivets. Good correlation of the fatigue crack growth data base obtained in this study and FASTRAN Code predictions show that the growth of MSD in the fuselage lap joint structure can be predicted by fracture mechanics based methods.
The Growth of Multi-Site Fatigue Damage in Fuselage Lap Joints
01.01.1999
Aufsatz (Konferenz)
Keine Angabe
Englisch
The Growth of Multi-Site Fatigue Damage in Fuselage Lap Joints
British Library Conference Proceedings | 1999
|Crack growth and repair of multi-site damage of fuselage lap joints
Tema Archiv | 1993
|British Library Conference Proceedings | 1999
|