Experimental investigation of lift for a wing-in-ground effect aircraft model
The aim of the investigation is to develop a technique of recalculating the lift as a function of the angle of attack at different reference points of the aircraft model height over the ground surface. A technique for evaluating the lift of the aircraft model close to the ground surface is proposed.
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| Veröffentlicht in: | Russian aeronautics 2016-04, Vol.59 (2), p.206-210 |
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| container_end_page | 210 |
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| container_issue | 2 |
| container_start_page | 206 |
| container_title | Russian aeronautics |
| container_volume | 59 |
| creator | Nazarov, D. V. Frolov, V. A. Shakhov, V. G. |
| description | The aim of the investigation is to develop a technique of recalculating the lift as a function of the angle of attack at different reference points of the aircraft model height over the ground surface. A technique for evaluating the lift of the aircraft model close to the ground surface is proposed. |
| doi_str_mv | 10.3103/S1068799816020082 |
| format | Article |
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| fulltext | fulltext |
| identifier | ISSN: 1068-7998 |
| ispartof | Russian aeronautics, 2016-04, Vol.59 (2), p.206-210 |
| issn | 1068-7998 1934-7901 |
| language | eng |
| recordid | cdi_crossref_primary_10_3103_S1068799816020082 |
| source | SpringerNature Journals |
| subjects | Aero- and Gas-Dynamics of Flight Vehicles and Their Engines Automotive Engineering Engineering |
| title | Experimental investigation of lift for a wing-in-ground effect aircraft model |
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