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An extension of the investigation of the effects of heat transfer on boundary-layer transition on a parabolic body of revolution (NACA RM-10) at a Mach number of 1.61
| Content Provider | University of North Texas |
|---|---|
| Author | Czarnecki, K. R. Sinclair, Archibald R. |
| Organization | Langley Aeronautical Laboratory |
| Description | Report presenting an investigation of the effects of heat transfer on boundary-layer transition at higher Reynolds numbers, greater amounts of heating, and a more extensive study of the effects of surface irregularities than what was published in a previous report. Report presenting tests with a smooth model and tests with surface roughness and tunnel flow disturbance are provided. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc57091 |
| Language | English |
| Publisher Date | 2018-06-04 |
| Access Restriction | Open |
| Subject Keyword | heat transfer effects boundary layer transition |
| Content Type | Text |
| Resource Type | Report |
