Effect of rivet or bolt holes on the ultimate strength developed by 24S-T and alclad 75S-T sheet in incomplete diagonal tension / by L. Ross Levin and David H. Nelson.
Series InformationTechnical note (United States. National Advisory Committee for Aeronautics) ; no. 1177.
- Physical Description: 1 online resource (10 pages, 6 unnumbered pages) : illustrations.
- Publisher: Washington : National Advisory Committee for Aeronautics, January 1947.
Distribution made by issuing office.
|Bibliography, etc. Note:||
Includes bibliographical references (page 9).
|Source of Description Note:||
Description based on online resource, PDF version; title from cover (NASA, viewed Feb. 23, 2018).