Effects of sweep and angle of attack on boundary-layer transition on wings at Mach number 4.04
| Author: | Dunning, Robert W |
|---|---|
| Year: | 1955 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-3473 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc57698/ |