Aerodynamic research in the wind tunnel on a gyroplane model
Artykuł w czasopiśmie
MNiSW
100
Lista 2024
| Status: | |
| Autorzy: | Fiedoruk Piotr, Łusiak Tomasz, Dudziak Jacek |
| Dyscypliny: | |
| Aby zobaczyć szczegóły należy się zalogować. | |
| Rok wydania: | 2026 |
| Wersja dokumentu: | Elektroniczna |
| Język: | angielski |
| Numer czasopisma: | 7 |
| Wolumen/Tom: | 20 |
| Strony: | 197 - 209 |
| Impact Factor: | 1,5 |
| Web of Science® Times Cited: | 0 |
| Scopus® Cytowania: | 0 |
| Bazy: | Web of Science | Scopus |
| Efekt badań statutowych | NIE |
| 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: | 1 czerwca 2026 |
| Abstrakty: | angielski |
| This paper presents the results of an experimental investigation of a gyroplane model conducted in a low‑speed wind tunnel. The primary objective of the study was to evaluate the aerodynamic characteristics of the complete configuration and selected partial configurations, including the cases without horizontal and vertical stabilisers. Measurements were performed for a range of fuselage angles of attack and sideslip angles to determine the influ- ence of landing gear deployment, nacelle geometry, and tail surfaces on aerodynamic performance. The analysis included the assessment of lift, drag, and side force coefficients, as well as stability and control derivatives. The results indicated that the horizontal stabiliser provides sufficient longitudinal stability, as confirmed by the calcu- lated Tail Volume Coefficient, while the nacelle form drag contributes significantly to the overall fuselage drag. Recommendations for future design improvements include optimization of nacelle shape and landing gear fairings to minimise drag and enhance lift during critical flight phases. |
