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: | Научный вестник МГТУ ГА |
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| Online Access: | https://avia.mstuca.ru/jour/article/view/618 |
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| _version_ | 1849408646158483456 |
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| author | M. V. Kondalov |
| author_facet | M. V. Kondalov |
| author_sort | M. V. Kondalov |
| collection | DOAJ |
| description | 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 of a deflection of mechanization of a wing for increase of aerodynamic quality of the aircraft. The calculation of flight range and duration was at incremental extension and at realization of adaptive deflection of nose flap for Mach number M < 0.6. |
| format | Article |
| id | doaj-art-5ee684106af94543a8dfd7c6caa07d5e |
| institution | Kabale University |
| issn | 2079-0619 2542-0119 |
| language | Russian |
| publishDate | 2016-11-01 |
| publisher | Moscow State Technical University of Civil Aviation |
| record_format | Article |
| series | Научный вестник МГТУ ГА |
| spelling | doaj-art-5ee684106af94543a8dfd7c6caa07d5e2025-08-20T03:35:44ZrusMoscow State Technical University of Civil AviationНаучный вестник МГТУ ГА2079-06192542-01192016-11-01020196104618ADAPTIVE DEFLECTION OF WING NOSE FLAP OF COMBAT TRAINING AIRCRAFT AND ITS IMPACT ON FLIGHT RANGE AND DURATIONM. V. Kondalov0ВУНЦ ВВС «ВВА им. проф. Н.Е. Жуковского и Ю.А. Гагарина»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 of a deflection of mechanization of a wing for increase of aerodynamic quality of the aircraft. The calculation of flight range and duration was at incremental extension and at realization of adaptive deflection of nose flap for Mach number M < 0.6.https://avia.mstuca.ru/jour/article/view/618combat training aircraftthe discrete vortex methodhigh lift systemaerodynamic quality |
| spellingShingle | M. V. Kondalov ADAPTIVE DEFLECTION OF WING NOSE FLAP OF COMBAT TRAINING AIRCRAFT AND ITS IMPACT ON FLIGHT RANGE AND DURATION Научный вестник МГТУ ГА combat training aircraft the discrete vortex method high lift system aerodynamic quality |
| title | ADAPTIVE DEFLECTION OF WING NOSE FLAP OF COMBAT TRAINING AIRCRAFT AND ITS IMPACT ON FLIGHT RANGE AND DURATION |
| title_full | ADAPTIVE DEFLECTION OF WING NOSE FLAP OF COMBAT TRAINING AIRCRAFT AND ITS IMPACT ON FLIGHT RANGE AND DURATION |
| title_fullStr | ADAPTIVE DEFLECTION OF WING NOSE FLAP OF COMBAT TRAINING AIRCRAFT AND ITS IMPACT ON FLIGHT RANGE AND DURATION |
| title_full_unstemmed | ADAPTIVE DEFLECTION OF WING NOSE FLAP OF COMBAT TRAINING AIRCRAFT AND ITS IMPACT ON FLIGHT RANGE AND DURATION |
| title_short | ADAPTIVE DEFLECTION OF WING NOSE FLAP OF COMBAT TRAINING AIRCRAFT AND ITS IMPACT ON FLIGHT RANGE AND DURATION |
| title_sort | adaptive deflection of wing nose flap of combat training aircraft and its impact on flight range and duration |
| topic | combat training aircraft the discrete vortex method high lift system aerodynamic quality |
| url | https://avia.mstuca.ru/jour/article/view/618 |
| work_keys_str_mv | AT mvkondalov adaptivedeflectionofwingnoseflapofcombattrainingaircraftanditsimpactonflightrangeandduration |