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Effects of eccentricities and lateral pressure on the design of stiffened compression panels

Author: Gary L Giles; Melvin S Anderson; Langley Research Center.; United States. National Aeronautics and Space Administration.
Publisher: Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va.] : [For sale by the National Technical Information Service], 1972.
Series: NASA technical note, D-6784.
Edition/Format:   Print book : National government publication : EnglishView all editions and formats
Summary:
An analysis for determining the effects of eccentricities and lateral pressure on the design of stiffened compression panels is presented. The four types of panel stiffeners considered are integral, zee, integral zee, and integral tee. Mass-strength curves, which give the mass of the panel necessary to carry a specified load, are given along with related design equations needed to calculate the cross-sectional  Read more...
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Additional Physical Format: Online version:
Giles, Gary L.
Effects of eccentricities and lateral pressure on the design of stiffened compression panels.
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972
(OCoLC)890699714
Material Type: Government publication, National government publication, Internet resource
Document Type: Book, Internet Resource
All Authors / Contributors: Gary L Giles; Melvin S Anderson; Langley Research Center.; United States. National Aeronautics and Space Administration.
OCLC Number: 680476927
Notes: Cover title.
Prepared at Langley Research Center.
Description: 33 pages : illustrations ; 27 cm.
Series Title: NASA technical note, D-6784.
Responsibility: by Gary L. Giles and Melvin S. Anderson.

Abstract:

An analysis for determining the effects of eccentricities and lateral pressure on the design of stiffened compression panels is presented. The four types of panel stiffeners considered are integral, zee, integral zee, and integral tee. Mass-strength curves, which give the mass of the panel necessary to carry a specified load, are given along with related design equations needed to calculate the cross-sectional dimensions of the minimum-mass-stiffened panel. The results of the study indicate that the proportions of the panels are geometrically similar to the proportions of panels designed for no eccentricity or lateral pressure, but no cross-sectional dimensions are greater, resulting in significantly increased mass. The analytical minimum-mass designs of zee-stiffened panels are compared with designs from experimentally derived charts. An assumed eccentricity of 0.001 times the length of the panel is used to correlate the analytical and experimental data. Good correlation between the experimentally derived and the analytical curves is obtained for the range of loading where materials yield governs the design. At lower loads the mass given by the analytical curve using this assumed eccentricity is greater than that given by the experimental results.

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Primary Entity<\/h3>\n
<http:\/\/www.worldcat.org\/oclc\/680476927<\/a>> # Effects of eccentricities and lateral pressure on the design of stiffened compression panels<\/span>\n\u00A0\u00A0\u00A0\u00A0a \nschema:Book<\/a>, schema:CreativeWork<\/a> ;\u00A0\u00A0\u00A0\nlibrary:oclcnum<\/a> \"680476927<\/span>\" ;\u00A0\u00A0\u00A0\nlibrary:placeOfPublication<\/a> <http:\/\/experiment.worldcat.org\/entity\/work\/data\/23007731#Place\/washington_d_c<\/a>> ; # Washington, D.C.<\/span>\n\u00A0\u00A0\u00A0\nlibrary:placeOfPublication<\/a> <http:\/\/id.loc.gov\/vocabulary\/countries\/dcu<\/a>> ;\u00A0\u00A0\u00A0\nlibrary:placeOfPublication<\/a> <http:\/\/experiment.worldcat.org\/entity\/work\/data\/23007731#Place\/springfield_va<\/a>> ; # Springfield, Va.<\/span>\n\u00A0\u00A0\u00A0\nschema:about<\/a> <http:\/\/id.worldcat.org\/fast\/1134288<\/a>> ; # Strains and stresses<\/span>\n\u00A0\u00A0\u00A0\nschema:about<\/a> <http:\/\/id.worldcat.org\/fast\/904190<\/a>> ; # Elastic plates and shells<\/span>\n\u00A0\u00A0\u00A0\nschema:about<\/a> <http:\/\/id.worldcat.org\/fast\/1066785<\/a>> ; # Plates (Engineering)<\/span>\n\u00A0\u00A0\u00A0\nschema:about<\/a> <http:\/\/id.worldcat.org\/fast\/901268<\/a>> ; # Eccentric loads<\/span>\n\u00A0\u00A0\u00A0\nschema:bookFormat<\/a> bgn:PrintBook<\/a> ;\u00A0\u00A0\u00A0\nschema:contributor<\/a> <http:\/\/viaf.org\/viaf\/146202023<\/a>> ; # United States. National Aeronautics and Space Administration.<\/span>\n\u00A0\u00A0\u00A0\nschema:contributor<\/a> <http:\/\/viaf.org\/viaf\/127305149<\/a>> ; # Langley Research Center.<\/span>\n\u00A0\u00A0\u00A0\nschema:contributor<\/a> <http:\/\/viaf.org\/viaf\/62949292<\/a>> ; # Melvin S. Anderson<\/span>\n\u00A0\u00A0\u00A0\nschema:creator<\/a> <http:\/\/viaf.org\/viaf\/6205593<\/a>> ; # Gary L. Giles<\/span>\n\u00A0\u00A0\u00A0\nschema:datePublished<\/a> \"1972<\/span>\" ;\u00A0\u00A0\u00A0\nschema:description<\/a> \"An analysis for determining the effects of eccentricities and lateral pressure on the design of stiffened compression panels is presented. The four types of panel stiffeners considered are integral, zee, integral zee, and integral tee. Mass-strength curves, which give the mass of the panel necessary to carry a specified load, are given along with related design equations needed to calculate the cross-sectional dimensions of the minimum-mass-stiffened panel. The results of the study indicate that the proportions of the panels are geometrically similar to the proportions of panels designed for no eccentricity or lateral pressure, but no cross-sectional dimensions are greater, resulting in significantly increased mass. The analytical minimum-mass designs of zee-stiffened panels are compared with designs from experimentally derived charts. An assumed eccentricity of 0.001 times the length of the panel is used to correlate the analytical and experimental data. Good correlation between the experimentally derived and the analytical curves is obtained for the range of loading where materials yield governs the design. 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<http:\/\/id.worldcat.org\/fast\/1134288<\/a>> # Strains and stresses<\/span>\n\u00A0\u00A0\u00A0\u00A0a \nschema:Intangible<\/a> ;\u00A0\u00A0\u00A0\nschema:name<\/a> \"Strains and stresses<\/span>\"@en<\/a> ;\u00A0\u00A0\u00A0\u00A0.\n\n\n<\/div>\n
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<http:\/\/viaf.org\/viaf\/6205593<\/a>> # Gary L. Giles<\/span>\n\u00A0\u00A0\u00A0\u00A0a \nschema:Person<\/a> ;\u00A0\u00A0\u00A0\nschema:familyName<\/a> \"Giles<\/span>\" ;\u00A0\u00A0\u00A0\nschema:givenName<\/a> \"Gary L.<\/span>\" ;\u00A0\u00A0\u00A0\nschema:name<\/a> \"Gary L. Giles<\/span>\" ;\u00A0\u00A0\u00A0\u00A0.\n\n\n<\/div>\n
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