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=81 tpl=download-button \/]<\/p>\n","protected":false},"excerpt":{"rendered":"Derives the principle strains in a laminate element given the ABD laminate properties and the input loads.","protected":false},"author":1,"featured_media":591,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[10],"tags":[],"aioseo_notices":[],"_links":{"self":[{"href":"https:\/\/xl-viking.com\/wp-json\/wp\/v2\/posts\/590"}],"collection":[{"href":"https:\/\/xl-viking.com\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/xl-viking.com\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/xl-viking.com\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/xl-viking.com\/wp-json\/wp\/v2\/comments?post=590"}],"version-history":[{"count":3,"href":"https:\/\/xl-viking.com\/wp-json\/wp\/v2\/posts\/590\/revisions"}],"predecessor-version":[{"id":1860,"href":"https:\/\/xl-viking.com\/wp-json\/wp\/v2\/posts\/590\/revisions\/1860"}],"wp:featuredmedia":[{"embeddable":true,"href":"https:\/\/xl-viking.com\/wp-json\/wp\/v2\/media\/591"}],"wp:attachment":[{"href":"https:\/\/xl-viking.com\/wp-json\/wp\/v2\/media?parent=590"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/xl-viking.com\/wp-json\/wp\/v2\/categories?post=590"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/xl-viking.com\/wp-json\/wp\/v2\/tags?post=590"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}
\nGeneral Method<\/p>\n
\nDerives the principle strains in a laminate element given the ABD laminate properties and the input loads.<\/p>\n