A Benchmark Example for Delamination Growth Predictions Based on the Single Leg Bending Specimen Under Fatigue LoadingAnalysis benchmarking is used to evaluate new algorithms for automated VCCT-based delamination growth analysis. First, existing benchmark cas s based on the Single Leg Bending (SLB) specimen for crack propagation prediction under quasi-static loading are summarized. Second, the development of new SLB-based benchmark cases to assess the static and fatigue growth prediction capabilities under mixed-mode I/II conditions is discussed in detail. Additionally, a scheme is proposed to interpolate between known fatigue delamination growth rates to obtain values for mixed-mode ratios for which data has not been defined in the input. Further, a comparison is presented, in which the benchmark cases are used to assess new analysis tools in ABAQUS/Standard FD03. These recently implemented tools yield results that are in good agreement with the benchmark examples. The ability to assess the implementation of new methods in one finite element code illustrates the value of establishing benchmark solutions.
Document ID
20200002622
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Krueger, Ronald (National Inst. of Aerospace Hampton, VA, United States)
Deobald, Lyle (Boeing Company Hampton, VA, United States)
Gu, Haozhong (Boeing Company Hampton, VA, United States)
Date Acquired
April 17, 2020
Publication Date
June 17, 2019
Subject Category
Composite MaterialsStructural Mechanics
Report/Patent Number
NF1676L-31543Report Number: NF1676L-31543
Meeting Information
Meeting: NAFEMS World Congress
Location: Quebec
Country: Canada
Start Date: June 17, 2019
End Date: June 20, 2019
Sponsors: National Agency for Finite Element Methods and Standards