Euler Solutions for a Medium-Range Cargo Aircraft
Computational fluid dynamics has advanced rapidly as a discipline and is being increasingly used to complement the wind-tunnel measurements of complete aircraft configurations. wind-tunnel tests are often limited by instrumentation constraints, precise model manufacturing, tunnel calibration, flow q...
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| Veröffentlicht in: | Journal of aircraft 2003-03, Vol.40 (2), p.393-395 |
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| Hauptverfasser: | , , , |
| Format: | Artikel |
| Sprache: | eng |
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| container_end_page | 395 |
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| container_issue | 2 |
| container_start_page | 393 |
| container_title | Journal of aircraft |
| container_volume | 40 |
| creator | Bahar, Cengizhan Alemdaroglu, Nafiz Ozyoruk, Yusuf Temel, Emre |
| description | Computational fluid dynamics has advanced rapidly as a discipline and is being increasingly used to complement the wind-tunnel measurements of complete aircraft configurations. wind-tunnel tests are often limited by instrumentation constraints, precise model manufacturing, tunnel calibration, flow quality, wall and support interferences, and aeroelastic effects. |
| doi_str_mv | 10.2514/2.3107 |
| format | Article |
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| fulltext | fulltext |
| identifier | ISSN: 0021-8669 |
| ispartof | Journal of aircraft, 2003-03, Vol.40 (2), p.393-395 |
| issn | 0021-8669 1533-3868 |
| language | eng |
| recordid | cdi_proquest_miscellaneous_27835688 |
| source | Alma/SFX Local Collection |
| subjects | Air transportation and traffic Aircraft Analysis Applied sciences Exact sciences and technology Fluid dynamics Ground, air and sea transportation, marine construction |
| title | Euler Solutions for a Medium-Range Cargo Aircraft |
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