NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Innovative design of composite structures: Design, manufacturing, and testing of plates utilizing curvilinear fiber trajectoriesAs a means of improving structural design, the concept of fabricating flat plates containing holes by incorporating curvilinear fiber trajectories to transmit loads around the hole is studied. In the present discussion this concept is viewed from a structural level, where access holes, windows, doors, and other openings are of significant size. This is opposed to holes sized for mechanical fasteners. Instead of cutting the important load-bearing fibers at the hole edge, as a conventional straightline design does, the curvilinear design preserves the load-bearing fibers by orienting them in smooth trajectories around the holes, their loading not ending abruptly at the hole edge. Though the concept of curvilinear fiber trajectories has been studied before, attempts to manufacture and test such plates have been limited. This report describes a cooperative effort between Cincinnati Milacron Inc., NASA Langley Research Center, and Virginia Polytechnic Institute and State University to design, manufacture, and test plates using the curvilinear fiber trajectory concept. The paper discusses details of the plate design, details of the manufacturing, and a summary of results from testing the plates with inplane compressive buckling loads and tensile loads. Comparisons between the curvilinear and conventional straightline fiber designs based on measurements and observation are made. Failure modes, failure loads, strains, deflections, and other key responses are compared.
Document ID
19950008451
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Hyer, M. W.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Rust, R. J.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Waters, W. A., Jr.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1994
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-197045
NAS 1.26:197045
VPI-E-94-08
Report Number: NASA-CR-197045
Report Number: NAS 1.26:197045
Report Number: VPI-E-94-08
Meeting Information
Meeting: DOD/NASA/FAA Conference on Fibrous Composites in Structural Design
Start Date: April 1, 1994
Accession Number
95N14865
Funding Number(s)
CONTRACT_GRANT: NAG1-901
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available