| タイトル | Turbulent Supersonic/Hypersonic Heating Correlations for Open and Closed Cavities |
| 本文（外部サイト） | http://hdl.handle.net/2060/20100033678 |
| 著者（英） | Everhart, Joel L.; Greene, Francis A. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2009-01-01 |
| 言語 | eng |
| 内容記述 | Supersonic/hypersonic laminar heating correlations that were developed for damage assessment analysis of atmospheric re-entry vehicles have been modified and extended to cover fully-turbulent conditions over rectangular cavity geometries that are aligned with the local velocity. Turbulent boundary layer properties were computationally determined and used to develop the cavity geometry parametrics and to correlate experimental closed cavity heating data to yield new relationships for the floor-averaged and centerline endwall peakheating augmentation. With the form of the closed-cavity correlations established, historical data were used to develop new correlations for turbulent open-cavity heating. |
| NASA分類 | Fluid Mechanics and Thermodynamics |
| レポートNO | LF99-8521 |
| 権利 | No Copyright |
