The Results of Wind-Tunnel Tests at Low Speeds 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: | Buell, Donald A. |
| Year: | 1953 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A53I28 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59893/ |