Effect of rivet or bolt holes on the ultimate strength developed by 24S-T and alclad 75S-T sheet in incomplete diagonal tension /
| Main Authors: | , |
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| Format: | Government Document eBook |
| Language: | English |
| Published: |
Washington :
National Advisory Committee for Aeronautics,
January 1947.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 1177. |
| Subjects: | |
| Online Access: | https://purl.fdlp.gov/GPO/gpo89368 |
Internet
https://purl.fdlp.gov/GPO/gpo89368Available Online
| Call Number: |
Y 3.N 21/5:1177 |
|
|---|---|---|
| Call Number | Status | Get It |
| Y 3.N 21/5:1177 | Available | |