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=65 tpl=download-button \/]<\/p>\n","protected":false},"excerpt":{"rendered":"A method to calculate the shear and bending moment distribution in a beam under axial compression and a UDL out of axis load.","protected":false},"author":1,"featured_media":543,"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\/542"}],"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=542"}],"version-history":[{"count":2,"href":"https:\/\/xl-viking.com\/wp-json\/wp\/v2\/posts\/542\/revisions"}],"predecessor-version":[{"id":1268,"href":"https:\/\/xl-viking.com\/wp-json\/wp\/v2\/posts\/542\/revisions\/1268"}],"wp:featuredmedia":[{"embeddable":true,"href":"https:\/\/xl-viking.com\/wp-json\/wp\/v2\/media\/543"}],"wp:attachment":[{"href":"https:\/\/xl-viking.com\/wp-json\/wp\/v2\/media?parent=542"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/xl-viking.com\/wp-json\/wp\/v2\/categories?post=542"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/xl-viking.com\/wp-json\/wp\/v2\/tags?post=542"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}
\nNiu Chapter 10<\/p>\n
\nA method to calculate the shear and bending moment distribution in a beam under axial compression and a UDL out of axis load. This method takes into account the deflection of the beam on the internal load distribution.<\/p>\n