Email this article Numerical Modeling of Helicopter Main Rotor Behavior near a Small-Scale Helideck by the Vortex Method
- Authors: Aparinov A.A.1, Kritskii B.S.1, Setukha A.V.1
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Affiliations:
- Zhukovsky Central Aerohydrodynamics Institute (TsAGI)
- Issue: Vol 60, No 4 (2017)
- Pages: 500-507
- Section: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journal-vniispk.ru/1068-7998/article/view/230264
- DOI: https://doi.org/10.3103/S1068799817040043
- ID: 230264
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Abstract
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.
Keywords
About the authors
A. A. Aparinov
Zhukovsky Central Aerohydrodynamics Institute (TsAGI)
Email: kritsky@starlink.ru
Russian Federation, ul. Zhukovskogo 1, Zhukovsky, 140181
B. S. Kritskii
Zhukovsky Central Aerohydrodynamics Institute (TsAGI)
Author for correspondence.
Email: kritsky@starlink.ru
Russian Federation, ul. Zhukovskogo 1, Zhukovsky, 140181
A. V. Setukha
Zhukovsky Central Aerohydrodynamics Institute (TsAGI)
Email: kritsky@starlink.ru
Russian Federation, ul. Zhukovskogo 1, Zhukovsky, 140181
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