Compressive Loading and Modeling of Stitched Composite StiffenersA series of single-frame and single-stringer compression tests were conducted at NASA Langley Research Center on specimens harvested from a large panel built using the Pultruded Rod Stitched Efficient Unitized Structure (PRSEUS) concept. Different frame and stringer designs were used in fabrication of the PRSEUS panel. In this paper, the details of the experimental testing of single-frame and single-stringer compression specimens are presented, as well as discussions on the performance of the various structural configurations included in the panel. Nonlinear finite element models were developed to further understand the failure processes observed during the experimental campaign.
Document ID
20160007734
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Leone, Frank A., Jr. (NASA Langley Research Center Hampton, VA, United States)
Jegley, Dawn C. (NASA Langley Research Center Hampton, VA, United States)
Linton, Kim A. (Boeing Co. Seal Beach, CA, United States)
Date Acquired
June 20, 2016
Publication Date
January 4, 2016
Subject Category
Aircraft Design, Testing And PerformanceStructural Mechanics
Report/Patent Number
NF1676L-21703Report Number: NF1676L-21703
Meeting Information
Meeting: AIAA Science and Technology Forum and Exposition
Location: San Diego, CA
Country: United States
Start Date: January 4, 2016
End Date: January 8, 2016
Sponsors: American Inst. of Aeronautics and Astronautics