Divergent-trailing-edge airfoil flow
Thompson and Lotz provide insight into the relationship between the structure of the recirculating flow in the vicinity of the blunt trailing edge and the drag reduction measured for divergent-trailing-edge (DTE) airfoils. DTE modification effects an increase in the streamwise length of the recircul...
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| Veröffentlicht in: | Journal of aircraft 1996-09, Vol.33 (5), p.950-955 |
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| Format: | Artikel |
| Sprache: | eng |
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| container_end_page | 955 |
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| container_issue | 5 |
| container_start_page | 950 |
| container_title | Journal of aircraft |
| container_volume | 33 |
| creator | Thompson, Brian E Lotz, Robert D |
| description | Thompson and Lotz provide insight into the relationship between the structure of the recirculating flow in the vicinity of the blunt trailing edge and the drag reduction measured for divergent-trailing-edge (DTE) airfoils. DTE modification effects an increase in the streamwise length of the recirculation region downstream of a blunt trailing edge that acts like a chordwise extension to increase circulation. |
| doi_str_mv | 10.2514/3.47040 |
| format | Article |
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| fulltext | fulltext |
| identifier | ISSN: 0021-8669 |
| ispartof | Journal of aircraft, 1996-09, Vol.33 (5), p.950-955 |
| issn | 0021-8669 1533-3868 |
| language | eng |
| recordid | cdi_aiaa_journals_10_2514_3_47040 |
| source | Alma/SFX Local Collection |
| subjects | Aerodynamics Aircraft Applied fluid mechanics Exact sciences and technology Fluid dynamics Fundamental areas of phenomenology (including applications) Physics |
| title | Divergent-trailing-edge airfoil flow |
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