| タイトル | Approximate method of predicting heating on the windward side of Space Shuttle Orbiter and comparisons with flight data |
| 著者（英） | Hamilton, H. H., II |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1982-06-01 |
| 言語 | eng |
| 内容記述 | An approximate method is developed for predicting laminar and turbulent heating rates on the windward side of the Space Shuttle Orbiter for both the wind-tunnel and flight environments. The method is based on a 'local infinite swept cylinder' analysis and includes both equilibrium-air chemistry and variable boundary-layer-edge entropy. The method is validated by comparing with data from wind-tunnel experiments and from the first and second Space Shuttle flights both along the windward-symmetry plane and in a lateral direction off the symmetry plane. Agreement with the flight data is good from approximately 67 km (peak heating) downward. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 82A31853
AIAA PAPER 82-0823 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/410679 |
