ADAPTIVE DEFLECTION OF WING NOSE FLAP OF COMBAT TRAINING AIRCRAFT AND ITS IMPACT ON FLIGHT RANGE AND DURATION
In this article presented the main result of numerical investigation of ability to improve the aerodynamic perfection of modern combat training aircraft. To determine the aerodynamic characteristic was used the discrete vortex method with closed vortex frames. In the work was presented the algorithm...
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| Format: | Article |
| Language: | Russian |
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Moscow State Technical University of Civil Aviation
2016-11-01
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| Series: | Naučnyj Vestnik MGTU GA |
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| Online Access: | https://avia.mstuca.ru/jour/article/view/618 |