Effects of Surface Roughness and Extreme Cooling on Boundary-Layer Transition for 15 Degrees Cone-Cylinder in Free Flight at Mach Numbers to 7.6
| Author: | Rabb, Leonard |
|---|---|
| Year: | 1958 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NASA-TM-79867, NACA-RM-E57K19 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc53340/ |