Comparison between experimental and predicted downwash at a Mach number of 0.25 behind a wing-body combination having a triangular wing of aspect ratio of 2.0
| Author: | Sorensen, Norman E. |
|---|---|
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-3720 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc55958/ |