An Analytical Investigation of Propeller Whirl Flutter

Abdulkadir Yildiz, Musa Kucukali, Seher Eken

Araştırma sonucu: Kitap/Rapor/Konferans Bildirisinde BölümKonferans katkısıbilirkişi

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 dilİngilizce
Ana bilgisayar yayını başlığıProceedings of 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023
YayınlayanInstitute of Electrical and Electronics Engineers Inc.
ISBN (Elektronik)9798350323023
DOI'lar
Yayın durumuYayınlandı - 2023
Etkinlik10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023 - Istanbul, Turkey
Süre: 7 Haz 20239 Haz 2023

Yayın serisi

AdıProceedings of 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023

???event.eventtypes.event.conference???

???event.eventtypes.event.conference???10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023
Ülke/BölgeTurkey
ŞehirIstanbul
Periyot7/06/239/06/23

Bibliyografik not

Publisher Copyright:
© 2023 IEEE.

Parmak izi

An Analytical Investigation of Propeller Whirl Flutter' araştırma başlıklarına git. Birlikte benzersiz bir parmak izi oluştururlar.

Alıntı Yap