The results of wind-tunnel tests to a Mach number of 0.90 of a four-engine, propeller-driven airplane configuration having a wing with 40 degrees of sweepback and an aspect ratio of 10
| Author: | Edwards, George G. |
|---|---|
| Additional Authors: | Sutton, Fred B., Dickson, Jerald K. |
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-3789 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc56062/ |