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Free-Flight Determination of Boundary-Layer Transition and Heat Transfer for a Hemisphere-Cylinder at Mach Numbers to 5.6
| Content Provider | University of North Texas |
|---|---|
| Author | Krasnican, M. J. Wisniewski, R. J. |
| Organization | Lewis Flight Propulsion Laboratory |
| Description | Report presenting testing of a highly polished 9-inch-diameter hemisphere-cylinder in flight in order to obtain boundary-layer transition and heat-transfer data. Results regarding the free-stream conditions, pressure measurements, temperature measurements, heat-transfer measurements, and transition and transition parameters are provided. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc63610 |
| Language | English |
| Publisher Date | 2019-01-10 |
| Access Restriction | Open |
| Subject Keyword | aerodynamics hemisphere cylinders |
| Content Type | Text |
| Resource Type | Report |