Effect of variation in rivet diameter and pitch on the average stress at maximum load for 24S-T3 and 75S-T6 aluminum-alloy, flat, Z-stiffened panels that fail by local instability
| Author: | Dow, Norris F |
|---|---|
| Year: | 1950 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-2139 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc55474/ |