FAST SOLUTION OF TURBULENT SEPARATION BY STRAWN’S METHOD
A quasi-simultaneous viscous/inviscid interaction model and a new integral method are tested in connection with the prediction 2D incompressible turbulent separated boundary layer flows. The results are compared with experiments and other predictions. (AIAA)
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| Veröffentlicht in: | Nanjing University of Aeronautics and Astronautics, Transactions (1005-1120) Transactions (1005-1120), 1994-05, Vol.11 (1), p.110-113 |
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| container_end_page | 113 |
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| container_issue | 1 |
| container_start_page | 110 |
| container_title | Nanjing University of Aeronautics and Astronautics, Transactions (1005-1120) |
| container_volume | 11 |
| creator | Yin, Junfei |
| description | A quasi-simultaneous viscous/inviscid interaction model and a new integral method are tested in connection with the prediction 2D incompressible turbulent separated boundary layer flows. The results are compared with experiments and other predictions. (AIAA) |
| format | Article |
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| fulltext | fulltext |
| identifier | ISSN: 1005-1120 |
| ispartof | Nanjing University of Aeronautics and Astronautics, Transactions (1005-1120), 1994-05, Vol.11 (1), p.110-113 |
| issn | 1005-1120 |
| language | eng |
| recordid | cdi_proquest_miscellaneous_26394752 |
| source | Alma/SFX Local Collection |
| subjects | aerodynamics boundary computational diffuse flow interaction layer mode now separation trubulent two-dimensional viscous/inviscid |
| title | FAST SOLUTION OF TURBULENT SEPARATION BY STRAWN’S METHOD |
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