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> \u00a0[wpfilebase tag=file id=23 tpl=download-button \/]<\/p>\n","protected":false},"excerpt":{"rendered":"Calculates Section Properties for Composite Rectangular Sections at any angle.","protected":false},"author":1,"featured_media":356,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":[],"categories":[10],"tags":[],"aioseo_notices":[],"_links":{"self":[{"href":"https:\/\/xl-viking.com\/wp-json\/wp\/v2\/posts\/349"}],"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=349"}],"version-history":[{"count":3,"href":"https:\/\/xl-viking.com\/wp-json\/wp\/v2\/posts\/349\/revisions"}],"predecessor-version":[{"id":1220,"href":"https:\/\/xl-viking.com\/wp-json\/wp\/v2\/posts\/349\/revisions\/1220"}],"wp:featuredmedia":[{"embeddable":true,"href":"https:\/\/xl-viking.com\/wp-json\/wp\/v2\/media\/356"}],"wp:attachment":[{"href":"https:\/\/xl-viking.com\/wp-json\/wp\/v2\/media?parent=349"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/xl-viking.com\/wp-json\/wp\/v2\/categories?post=349"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/xl-viking.com\/wp-json\/wp\/v2\/tags?post=349"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}
\nNon Specific, General Method<\/p>\n
\nCalculates Section Properties for Composite Rectangular Sections at any angle. Includes simple moment distribution about two axes and end load distribution.<\/p>\n