Özet
The advent of novel electric-powered propeller aircraft designs brings back increased focus on assessment of aircraft whirl flutter. During operation of propeller-driven aircraft, generation of aerodynamic forces on the propeller blades and their interaction with the inertial and elastic forces of the blades cause this phenomenon. In this study, an analytical model is presented for the solution of whirl flutter of propellerengine system. The engine-propeller configuration is assumed to be rigid, while it is flexibly mounted to undergo angular displacement in the vertical (pitch) plane of the propeller axis and in the horizontal (yaw) plane. The stability characteristics of the presented model is analytically investigated and plotted for varying advance ratio values.
Orijinal dil | İngilizce |
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Ana bilgisayar yayını başlığı | Proceedings of 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023 |
Yayınlayan | Institute of Electrical and Electronics Engineers Inc. |
ISBN (Elektronik) | 9798350323023 |
DOI'lar | |
Yayın durumu | Yayınlandı - 2023 |
Etkinlik | 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023 - Istanbul, Turkey Süre: 7 Haz 2023 → 9 Haz 2023 |
Yayın serisi
Adı | Proceedings of 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023 |
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???event.eventtypes.event.conference??? | 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023 |
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Ülke/Bölge | Turkey |
Şehir | Istanbul |
Periyot | 7/06/23 → 9/06/23 |
Bibliyografik not
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