Enviar artigo por via de e-mail Numerical Modeling of Helicopter Main Rotor Behavior near a Small-Scale Helideck by the Vortex Method
- Autores: Aparinov A.A.1, Kritskii B.S.1, Setukha A.V.1
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Afiliações:
- Zhukovsky Central Aerohydrodynamics Institute (TsAGI)
- Edição: Volume 60, Nº 4 (2017)
- Páginas: 500-507
- Seção: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230264
- DOI: https://doi.org/10.3103/S1068799817040043
- ID: 230264
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Resumo
A mathematical model and numerical scheme of the method being used are described. The results of calculating the helicopter main rotor aerodynamic performance in hover mode above a helideck are compared to the known wind tunnel test data.
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Sobre autores
A. Aparinov
Zhukovsky Central Aerohydrodynamics Institute (TsAGI)
Email: kritsky@starlink.ru
Rússia, ul. Zhukovskogo 1, Zhukovsky, 140181
B. Kritskii
Zhukovsky Central Aerohydrodynamics Institute (TsAGI)
Autor responsável pela correspondência
Email: kritsky@starlink.ru
Rússia, ul. Zhukovskogo 1, Zhukovsky, 140181
A. Setukha
Zhukovsky Central Aerohydrodynamics Institute (TsAGI)
Email: kritsky@starlink.ru
Rússia, ul. Zhukovskogo 1, Zhukovsky, 140181
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