Визначення аеродинамічних характеристик конвертоплана з розміщеними на кінцях крила співвісними гвинтовими рушіями
| dc.contributor.author | Поваров, С. А. | |
| dc.date.accessioned | 2023-04-27T12:08:41Z | |
| dc.date.available | 2023-04-27T12:08:41Z | |
| dc.date.issued | 2020 | |
| dc.description.abstractother | The article describes the study of rotor-to-wing aerodynamic interaction for the wingtip-mounted coaxial rotors configuration of the tiltrotor aircraft. The influence of the rotor slipstreams on lift-to-drag ratio characteristic was determined. Obtained results were compared with similar characteristics of the equivalent in thrust conventional single rotor slipstreams impact. Using the computational aerodynamics methods (panel-vortex method) the flow around the tiltrotor model with the wingtip-mounted single and coaxial rotors has been simulated. A study of the basic model configuration with conventional single rotors, based on the technical characteristics of the AgustaWestland AW609 tiltrotor, was conducted. Further researches were conducted for a modified model where single rotors were replaced with equivalent in thrust coaxial rotors. The influence of the rotor slipstreams on the aerodynamic characteristics of the model for both directions of rotors rotation in coaxial combination is considered. Also, the dependence of the maximum lift-to-drag characteristic due to the coaxial rotor diameters change has been determined. The results show that the coaxial rotor slipstreams-to-wing aerodynamic interaction effect is the similar to the effect of conventional single rotor, but less intensive. Comparison of the results showed that a tiltrotor equipped with wingtipmounted single rotors has approximately 20% greater maximum lift-to-drag characteristic than one equipped with coaxial rotors with the same thrust. However, the use of coaxial rotors allows getting higher maximum speed, when conventional single rotors lose the efficiency significantly. Therefore, it is advisable to conduct further research for the possibility of using coaxial rotors for tiltrotor aircrafts. The research results are presented in graphical form. The obtained data provides a basis for further studies of the described problem, and also will be useful for new tiltrotor design works. | uk |
| dc.format.pagerange | С. 108-116 | uk |
| dc.identifier.citation | Поваров, С. А. Визначення аеродинамічних характеристик конвертоплана з розміщеними на кінцях крила співвісними гвинтовими рушіями / С. А. Поваров // Механіка гіроскопічних систем : науково-технічний збірник. – 2020. – Вип. 40. – С. 108-116. – Бібліогр.: 10 назв. | uk |
| dc.identifier.doi | https://doi.org/10.20535/0203-3771402020248778 | |
| dc.identifier.uri | https://ela.kpi.ua/handle/123456789/55049 | |
| dc.language.iso | uk | uk |
| dc.publisher | КПІ ім. Ігоря Сікорського | uk |
| dc.publisher.place | Київ | uk |
| dc.relation.ispartof | Механіка гіроскопічних систем: науково-технічний збірник, Вип. 40 | uk |
| dc.subject.udc | 533.65.013.622 | uk |
| dc.title | Визначення аеродинамічних характеристик конвертоплана з розміщеними на кінцях крила співвісними гвинтовими рушіями | uk |
| dc.type | Article | uk |
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