Analysis of discrete-source damage progression in a tensile stiffened composite panel

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

Volumn 2, Issue , 1999, Pages 1174-1187

  Wang, John T ^a   Lotts, Christine G ^a   Sleight, David W ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPOSITE STRUCTURES; FAILURE (MECHANICAL); FINITE ELEMENT METHOD; STIFFNESS; TENSILE STRESS;

DAMAGE PROGRESSION ANALYSIS; DISCRETE SOURCE DAMAGE PROGRESSION; FAILURE CRITERIA; LARGE SCALE FIVE STRINGER COMPOSITE PANEL; MESH SIZES; SAW CUT MODELING;

STRUCTURAL PANELS;

EID: 0032643078     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Article

References (23)