Measurements of Aerodynamic Interference of a Hybrid Aircraft with Multirotor Propulsion
Artykuł w czasopiśmie
MNiSW
100
Lista 2021
| Status: | |
| Autorzy: | Czyż Zbigniew, Wendeker Mirosław |
| Dyscypliny: | |
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| Rok wydania: | 2020 |
| Wersja dokumentu: | Elektroniczna |
| Język: | angielski |
| Numer czasopisma: | 12 |
| Wolumen/Tom: | 20 |
| Numer artykułu: | 3360 |
| Strony: | 1 - 14 |
| Impact Factor: | 3,576 |
| Web of Science® Times Cited: | 3 |
| Scopus® Cytowania: | 9 |
| Bazy: | Web of Science | Scopus |
| Efekt badań statutowych | NIE |
| Finansowanie: | This work has been financed by the Polish National Centre for Research and Development under the LIDER program Grant Agreement No. LIDER/27/0140/L-10/18/NCBR/2019. |
| Materiał konferencyjny: | NIE |
| Publikacja OA: | TAK |
| Licencja: | |
| Sposób udostępnienia: | Witryna wydawcy |
| Wersja tekstu: | Ostateczna wersja opublikowana |
| Czas opublikowania: | W momencie opublikowania |
| Data opublikowania w OA: | 13 czerwca 2020 |
| Abstrakty: | angielski |
| This article deals with the phenomenon of aerodynamic interference occurring in theinnovative hybrid system of multirotor aircraft propulsion. The approach to aerodynamics requiresa determination of the impact of active sources of lift and thrust upon the aircraft aerodynamiccharacteristics. The hybrid propulsion unit, composed of a conventional multirotor source of thrust aswell as lift in the form of the main rotor and a pusher, was equipped with an additional propeller driveunit. The tests were conducted in a continuous-flow low speed wind tunnel with an open measuringspace, 1.5 m in diameter and 2.0 m long. Force testing made it possible to develop aerodynamiccharacteristics as well as defining aerodynamic characteristics and defining the field of speed forthe considered design configurations. Our investigations enabled us to analyze the results in termsof a mutual impact of particular components of the research object and the area of impact of activeelements present in a common flow. |
