Sample Engineering Spreadsheets Provided by Abbott Aerospace Inc<\/a><\/p>\n This spreadsheet uses the XL-Viking Plugin to display equations. The Spreadsheet will calculate correctly without the plugin and can be used ‘as is’ but none of the math will be visible. To find out more about XL-Viking click here<\/a>.<\/p>\n References:<\/strong> Description:<\/strong> [wpfilebase tag=file id=92 tpl=download-button \/]<\/p>\n","protected":false},"excerpt":{"rendered":"Methods for the stress analysis for small and large deflections on sandwich plates.","protected":false},"author":1,"featured_media":624,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":[],"categories":[10],"tags":[],"aioseo_notices":[],"_links":{"self":[{"href":"http:\/\/xl-viking.com\/wp-json\/wp\/v2\/posts\/623"}],"collection":[{"href":"http:\/\/xl-viking.com\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"http:\/\/xl-viking.com\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"http:\/\/xl-viking.com\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"http:\/\/xl-viking.com\/wp-json\/wp\/v2\/comments?post=623"}],"version-history":[{"count":2,"href":"http:\/\/xl-viking.com\/wp-json\/wp\/v2\/posts\/623\/revisions"}],"predecessor-version":[{"id":1297,"href":"http:\/\/xl-viking.com\/wp-json\/wp\/v2\/posts\/623\/revisions\/1297"}],"wp:featuredmedia":[{"embeddable":true,"href":"http:\/\/xl-viking.com\/wp-json\/wp\/v2\/media\/624"}],"wp:attachment":[{"href":"http:\/\/xl-viking.com\/wp-json\/wp\/v2\/media?parent=623"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"http:\/\/xl-viking.com\/wp-json\/wp\/v2\/categories?post=623"},{"taxonomy":"post_tag","embeddable":true,"href":"http:\/\/xl-viking.com\/wp-json\/wp\/v2\/tags?post=623"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}
\nNASA Structures Manual TM X-73305, Chapter B9.6 Structural Sandwich Plates, Subchapter B9.6.1.1 Basic Principles for Design of Flat Sandwich Panels under Uniformly Distributed Normal Load.
\nBruhn, Para. A17.7, Large Deflections Theory<\/p>\n
\nMethods for the stress analysis for small and large deflections on sandwich plates.<\/p>\n