| タイトル | Aerodynamic heating on complex configurations |
| 著者（英） | Dejarnette, F. R. |
| 著者所属（英） | North Carolina State Univ. |
| 発行日 | 1979-01-01 |
| 言語 | eng |
| 内容記述 | A relatively simple method was developed previously (DeJarnette and Hamilton, 1973; 1975) to calculate laminar transitional and turbulent heating rates on blunt bodies at angles of attack, taking into account entropy-swelling effects. The method has now been extended to include complex configurations and the use of input surface pressure data when available. Applications of the extended method to the HL-10 Lifting Body, a blunted tangent ogive, a blunted tangent-ogive cylinder, and the Viking Aeroshell are discussed. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 79A34723
AIAA PAPER 79-0891 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/427347 |
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