Stability and control characteristics of a complete airplane model having a wing with quarter-chord line swept back 40 degrees, aspect ratio 2.50, and taper ratio 0.42
| Author: | Schulderfrei, Marvin |
|---|---|
| Additional Authors: | Comisarow, Paul |
| Year: | 1951 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-2482 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc55718/ |