Aerodynamic analysis of the aircraft model made with the 3D printing method
Artykuł w czasopiśmie
MNiSW
5
spoza listy
| Status: | |
| Autorzy: | Iljaszewicz Paulina, Łusiak Tomasz, Pastuszak Anna, Novák Andrej |
| Dyscypliny: | |
| Aby zobaczyć szczegóły należy się zalogować. | |
| Rok wydania: | 2020 |
| Wersja dokumentu: | Drukowana | Elektroniczna |
| Język: | angielski |
| Wolumen/Tom: | 51 |
| Strony: | 118 - 133 |
| Scopus® Cytowania: | 4 |
| Bazy: | Scopus |
| Efekt badań statutowych | NIE |
| Materiał konferencyjny: | TAK |
| Nazwa konferencji: | INAIR 2020 - Challenges of Aviation Development |
| Skrócona nazwa konferencji: | INAIR 2020 |
| URL serii konferencji: | LINK |
| Termin konferencji: | 4 listopada 2020 do 5 listopada 2020 |
| Miasto konferencji: | Žylina |
| Państwo konferencji: | SŁOWACJA |
| Publikacja OA: | TAK |
| Licencja: | |
| Sposób udostępnienia: | Otwarte czasopismo |
| Wersja tekstu: | Ostateczna wersja opublikowana |
| Czas opublikowania: | W momencie opublikowania |
| Data opublikowania w OA: | 4 grudnia 2020 |
| Abstrakty: | angielski |
| The article presents an aerodynamic analysis of the aircraft model. The process of constructing the physical model began with the development of geometry. Preliminary design was made using SolidWorks program, giving the desired shape with as many details as the method allowed. It had to be made precisely, because later it was to be printed on a 3D printer. In this phase of the project a special hole was also prepared on the model side for mounting in the wind tunnel. Important conditions were measured and written down. The applied wind tunnel - Gunt HM 170 - enabled the measurement of the lifting forces and resistance at four different air speeds (15, 20, 25 and 28 m/s) and different angles of attack - 0˚, 2˚, 4˚, 6˚ ... 16˚ and then 0˚, -2˚, -4˚, -6˚ ... -12˚. On the basis of the results obtained, the load bearing force and resistance coefficients were calculated. In order to make a comparison, a simulation was prepared in the SolidWorks Flow Simulation, using the same conditions as in the wind tunnel test. This allowed for a relative comparison of the results from tests on physical models. The obtained results of uplift and resistance forces were tabulated. |
