Analysis 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: | Demele, Fred A., Buell, Donald A. |
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-3790 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc56014/ |