Boundary-layer transition on a cooled 20 degree cone at Mach numbers of 1.5 and 2.0
| Author: | Scherrer, Richard |
|---|---|
| Year: | 1950 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-2131 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc55639/ |