Preliminary results from a free-flight investigation of boundary-layer transition and heat transfer on a highly polished 8-inch-diameter hemisphere-cylinder at Mach numbers up to 3 and Reynolds numbers based on a length of 1 foot up to 17.7 x 10⁶
| Author: | Hall, J. R. |
|---|---|
| Additional Authors: | Piland, Robert O., Speegle, Katherine C. |
| Year: | 1957 |
| Document Type: | NACA |
| Issuing Agency: | National Advisory Committee for Aeronautics, |
| SUDOC: | Y 3.N21/5:15/L57D18c |
| Series: | NACA research memorandum ; |
| Report Number: | L57D18c |
| Subjects: | Heat--Transmission |
| Boundary layer | |
| Thermal boundary layer | |
| Link: | https://hdl.handle.net/2027/mdp.39015086507186 |