Linking riveting process parameters to the fatigue performance of riveted aircraft structures

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 2, Issue , 1999, Pages 1208-1218

  Szolwinski, M P ^a   Farris, T N ^a  

^a RENSSELAER POLYTECHNIC INSTITUTE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CRACK PROPAGATION; FATIGUE OF MATERIALS; FINITE ELEMENT METHOD; INTERFACES (MATERIALS); JOINTS (STRUCTURAL COMPONENTS); RESIDUAL STRESSES; RIVETING; RIVETS; STRUCTURAL LOADS;

INELASTIC RESPONSE; LINKING RIVETING PROCESS; RIVET HOLE INTERFACE; RIVETED AIRCRAFT STRUCTURES; SQUEEZE FORCE; WIDESPREAD FATIGUE DAMAGE;

AIRCRAFT;

EID: 0032690349     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-1339     Document Type: Article

References (19)