Innovative Design of Composite Structures: The Use of Curvilinear Fiber Format to Improve Buckling Resistance of Composite Plates with Central Circula

By: Nasa, National Aeronautics and Space Adm

The gains in buckling performance are explored that can be achieved by deviating from the conventional straightline fiber format and considering the situation whereby the fiber orientation in a layer, or a group of layers, can vary from point to point. The particular situation studied is a simply supported square plate with a centrally located hole loaded in compression. By using both a sensitivity analysis and a gradient-search technique, fiber orientation in a number of regions of the plate are selected so as to increase the buckling load relative to baseline straightline designs. The sensitivity analysis is used to determine which regions of the plate have the most influence on buckling load, and the gradient search is used to find the design that is believed to represent the absolute maximum buckling load for the conditions prescribed. Convergence studies and sensitivity of the final design are discussed. By examining the stress resultant contours, it is shown how the curvilinear fibers move the load away from the unsupported hole region of the plate to the supported edges, thus increasing the buckling capacity. The tensile capacity of the improved buckling design is investigated, and it is shown that both tensile capacity and buckling capacity can be improved with the curvilinear fiber concept. Hyer, M. W. and Lee, H. H. Unspecified Center NAG1-901...

• Format: Paperback
• Language: English
• ISBN: 1729029329
• ISBN13: 9781729029329
• Release Date: January 1
• Publisher: Independently Published
• Length: 28 Pages
• Weight: 0.48 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"