| タイトル | Application of an improved unified subsonic-supersonic potential flow method for the aerodynamic analysis of aircraft configurations |
| 著者（英） | Fox, C. H., Jr.; Breedlove, W. J., Jr. |
| 発行日 | 1974-01-01 |
| 言語 | eng |
| 内容記述 | F. A. Woodward, under contract to the NASA Langley Research Center, has recently formulated a distributed vortex aerodynamic singularity and developed an improved unified subsonic-supersonic potential flow computer program employing this singularity. This improved program is applicable to the prediction of the local surface pressure distribution for a large class of essentially arbitrarily shaped aircraft configurations. Results are presented for two classes of aircraft configurations of current interest: a maneuvering fighter type and a supersonic transport type. Comparison of these results with experiment indicate the program has good prediction capability. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 74A18841
AIAA PAPER 74-186 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/454053 |
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