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COMPARISON OF DIFFERENT IONOCRAFT ELECTRODE SYSTEM MODELS
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| dc.contributor | Казанский (Приволжский) федеральный университет | |
| dc.contributor.author | Dremin D.V. | ru_RU |
| dc.contributor.author | Khomich Yu.V. | ru_RU |
| dc.contributor.author | Rebrov I.E. | ru_RU |
| dc.date.accessioned | 2018-01-10T09:16:05Z | |
| dc.date.available | 2018-01-10T09:16:05Z | |
| dc.date.issued | 2017 | |
| dc.identifier.uri | http://dspace.kpfu.ru/xmlui/handle/net/117378 | |
| dc.description.abstract | The influence on thrust parameter and efficiency from geometric parameters and design features of the ionocraft electrode systems (IES) in air at atmospheric pressure and natural humidity is considered. Collector in form of a grid or two parallel tubes gives a significant increase of thrust and thrust-to-power ratio of EHD propulsion system compared with the single tube collector. | ru_RU |
| dc.relation.ispartofseries | "ФИЗИКА НИЗКОТЕМПЕРАТУРНОЙ ПЛАЗМЫ" ФНТП-2017 | ru_RU |
| dc.subject | - | ru_RU |
| dc.title | COMPARISON OF DIFFERENT IONOCRAFT ELECTRODE SYSTEM MODELS | ru_RU |
| dc.type | article | |
| dc.identifier.udk | - | |
| dc.description.pages | 242-242 |
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"ФИЗИКА НИЗКОТЕМПЕРАТУРНОЙ ПЛАЗМЫ" ФНТП-2017 [232]
материалы Всероссийской (с международным участием) конференции "Физика низкотемпературной плазмы" ФНТП-2017 (Казань,5 - 9 июня 2017 г), 05.06.2017-09.06.2017