Boundary-layer transition at high Reynolds numbers as obtained in flight of a 20 degree cone-cylinder with wall to local stream temperature ratios near 1.0
| Author: | Rabb, Leaonard |
|---|---|
| Year: | 1955 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E55I15 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc61627/ |