Postbuckling behavior of graphite/epoxy cloth shear panels with 45º-flanged lightening holes
dc.contributor.advisor | Bank, Milton Harold | |
dc.contributor.author | Herman, Richard John | |
dc.contributor.corporate | Naval Postgraduate School (U.S.) | |
dc.contributor.department | Aeronautics | |
dc.contributor.secondreader | Lindsey, G.S. | |
dc.date | March 1982 | |
dc.date.accessioned | 2012-11-20T00:08:29Z | |
dc.date.available | 2012-11-20T00:08:29Z | |
dc.date.issued | 1982-03 | |
dc.description.abstract | An experimental and finite-element analysis was performed on graphite/epoxy cloth plates subjected to static shear loading. Two specimens were tested to failure for each of three configurations: a solid panel, a panel with an unreinforced hole and a panel with a 45°-flanged hole. Both a static nonlinear analysis and a bifurcation-buckling analysis were performed for each of the panel configurations. The 45°-flange reinforcement technique for cutouts in shear webs was found to be well-suited for use in non-buckling, graphite/epoxy cloth designs. However, an alternate hole-reinforcement technique is required for designs where buckling is allowed. | |
dc.description.distributionstatement | Approved for public release; distribution is unlimited. | |
dc.description.service | Lieutenant Commander, United States Navy | |
dc.description.uri | http://archive.org/details/postbucklingbeha1094520302 | |
dc.identifier.uri | https://hdl.handle.net/10945/20302 | |
dc.language.iso | en_US | |
dc.publisher | Monterey, California. Naval Postgraduate School | en_US |
dc.rights | This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States. | |
dc.subject.author | Laminate | en_US |
dc.subject.author | Composite material | en_US |
dc.subject.author | Shear loading | en_US |
dc.subject.author | Hole reinforcement | en_US |
dc.subject.lcsh | Aeronautics | en_US |
dc.title | Postbuckling behavior of graphite/epoxy cloth shear panels with 45º-flanged lightening holes | en_US |
dc.type | Thesis | en_US |
dspace.entity.type | Publication | |
etd.thesisdegree.discipline | Aeronautical Engineering | en_US |
etd.thesisdegree.grantor | Naval Postgraduate School | en_US |
etd.thesisdegree.level | Masters | en_US |
etd.thesisdegree.name | M.S. in Aeronautical Engineering | en_US |
Files
Original bundle
1 - 1 of 1
Loading...
- Name:
- postbucklingbeha00herm.pdf
- Size:
- 13.96 MB
- Format:
- Adobe Portable Document Format