| タイトル | The effect of canard relative size and vertical location on the subsonic longitudinal and lateral-directional static aerodynamic characteristics for a model with a swept forward wing |
| 本文（外部サイト） | http://hdl.handle.net/2060/19790019967 |
| 著者（英） | Fox, C. H., Jr.; Huffman, J. K. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1979-07-01 |
| 言語 | eng |
| 内容記述 | A general research fighter model was tested in the Langley 7- by 10-foot high speed tunnel at a Mach number of 0.3. The model was tested with a 32 deg swept forward wing mounted in mid-, low-, and high-wing positions. For the mid-wing configuration, the model was tested with a 51.7 deg swept back canard mounted in mid-, low-, and high-canard positions. For the mid-wing mid-canard and the mid-wing high-canard configurations, canards of similar planform having two different areas were tested. The angle-of-attack range was from approximately -4 deg to 48 deg at sideslip angles of 0 deg, -5 deg, and 5 deg. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 79N28138
NASA-TM-78739 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/174994 |
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