Access the full text.
Sign up today, get DeepDyve free for 14 days.
References for this paper are not available at this time. We will be adding them shortly, thank you for your patience.
THIS problem is similar to that treated in section C, but now the stringers will be treated as discrete members separated by panels of skin which transmit only shear stress. The method of solution is quite different from that hitherto employed, it having been found that the result was most conveniently obtained by the principle of minimum strain energy. The problem is shown diagrammatically in FIG. 16, where the notation to be used is also given.
Aircraft Engineering and Aerospace Technology – Emerald Publishing
Published: Nov 1, 1946
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.