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Free-Flight Aerodynamic-Heating Data at Mach Numbers Up to 10.9 on a Flat-Faced Cylinder
| Content Provider | University of North Texas |
|---|---|
| Author | Bland, William M. Jr. Swanson, Andrew G. Kolenkiewicz, Ronald |
| Organization | Langley Aeronautical Laboratory |
| Description | Memorandum presenting a five-stage rocket-propelled model flown up to a Mach number of 10.9 and a corresponding free-stream Reynolds number of 6.57 x 10(exp 6) based on nose diameter. Temperatures were measured at 16 stations on the inside of a flat-faced cylinder made of copper. Results regarding the flight test, wall temperatures, heat-transfer data, measurement repeatibility and effects of angle of attack, comparison of measured and theoretical stagnation-point heating rates, and measured and theoretical heating rates over the front and side of the nose are provided. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc52904 |
| Language | English |
| Publisher Date | 2018-12-20 |
| Access Restriction | Open |
| Subject Keyword | aerodynamic heating flat-faced cylinders |
| Content Type | Text |
| Resource Type | Report |