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Progressive Damage Mechanisms in Thick 3D Composite Structures under Static and Fatigue LoadingThe objective of this work is to demonstrate validation of predictive capabilities
capturing both damage initiation and growth under static and fatigue loading in
geometrically complex three-dimensional (3D) composite structures. The composite
structure of interest in the present study resembles a 3D blade spar used in rotorcraft
applications. Under both static and fatigue testing, it was shown that damage initiated
at the same ply-drop location(s) and grew in the axial as well as hoop directions.
CompDam – a state-of-the-art Progressive Damage Analysis (PDA) tool was used to
achieve successful correlations of metrics including load-displacement responses and
damage modes.
Document ID
20205003616
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Prabhakar M. Rao
(Raytheon (United States) Waltham, Massachusetts, United States)
Mark R. Gurvich
(Raytheon (United States) Waltham, Massachusetts, United States)
Nalinda W. Waas
(Wichita State University Wichita, Kansas, United States)
Upul R. Palliyaguru
(Wichita State University Wichita, Kansas, United States)
Waruna Seneviratne
(Wichita State University Wichita, Kansas, United States)
Date Acquired
June 17, 2020
Subject Category
Composite Materials
Meeting Information
Meeting: ASC 35TH Technical Conference & ASTM D-30 Committee Meeting
Location: Stevens Institute of Technology
Country: US
Start Date: September 14, 2020
End Date: September 17, 2020
Sponsors: Stevens Institute of Technology
Funding Number(s)
WBS: 826611.04.07.01
CONTRACT_GRANT: NNL09AA00A
CONTRACT_GRANT: 80LARC17C0004
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
External Peer Committee
Keywords
progressive damage analysis
PDA
ACP
composites
ACC
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