Numerical Modeling of Helicopter Main Rotor Behavior near a Small-Scale Helideck by the Vortex Method


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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.

作者简介

A. Aparinov

Zhukovsky Central Aerohydrodynamics Institute (TsAGI)

Email: kritsky@starlink.ru
俄罗斯联邦, ul. Zhukovskogo 1, Zhukovsky, 140181

B. Kritskii

Zhukovsky Central Aerohydrodynamics Institute (TsAGI)

编辑信件的主要联系方式.
Email: kritsky@starlink.ru
俄罗斯联邦, ul. Zhukovskogo 1, Zhukovsky, 140181

A. Setukha

Zhukovsky Central Aerohydrodynamics Institute (TsAGI)

Email: kritsky@starlink.ru
俄罗斯联邦, ul. Zhukovskogo 1, Zhukovsky, 140181

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