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Applied sciences, v.7 no.9, 2017년, pp.918 -
Batrakov, Andrey (Aerohydrodynamics Department, Kazan National Research Technical University n.a. A.N. Tupolev (KNRTU-KAI), 10 Karl Marx St., Kazan 420111, Russia) , Kusyumov, Alexander (Aerohydrodynamics Department, Kazan National Research Technical University n.a. A.N. Tupolev (KNRTU-KAI), 10 Karl Marx St., Kazan 420111, Russia) , Kusyumov, Sergey (Aerohydrodynamics Department, Kazan National Research Technical University n.a. A.N. Tupolev (KNRTU-KAI), 10 Karl Marx St., Kazan 420111, Russia) , Mikhailov, Sergey (Aerohydrodynamics Department, Kazan National Research Technical University n.a. A.N. Tupolev (KNRTU-KAI), 10 Karl Marx St., Kazan 420111, Russia) , Barakos, George (School of Engineering, University of Glasgow, Glasgow G12 8QQ, UK)
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In this work, fully-resolved rotor-fuselage interactional aerodynamics is used as the forcing term in a model based on the Euler-Bernoulli equation, aiming to simulate helicopter tail-boom vibration. The model is based on linear beam analysis and captures the effect of the blade-passing as well as t...
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