Access the full text.
Sign up today, get DeepDyve free for 14 days.
TO check the suitability of a given strut crosssection, for a given length and safe concentric working load, is a simple matter provided that a working stress curve or formula is available, but the reverse process of obtaining a suitable crosssection, for a given length and load is under normal circumstances a tedious trial and error task, unless comprehensive tables of the properties of the required section arc available. The author's method permits a very close first approximation to be obtained, which is frequently sufficiently accurate to enable the required crosssection to be laid out without further trial.
Aircraft Engineering and Aerospace Technology – Emerald Publishing
Published: Aug 1, 1944
Read and print from thousands of top scholarly journals.
Already have an account? Log in
Bookmark this article. You can see your Bookmarks on your DeepDyve Library.
To save an article, log in first, or sign up for a DeepDyve account if you don’t already have one.
Copy and paste the desired citation format or use the link below to download a file formatted for EndNote
Access the full text.
Sign up today, get DeepDyve free for 14 days.
All DeepDyve websites use cookies to improve your online experience. They were placed on your computer when you launched this website. You can change your cookie settings through your browser.