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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
  • 1 Zhukovsky Central Aerohydrodynamics Institute (TsAGI), ul. Zhukovskogo 1, Zhukovsky, 140181, Russia , Zhukovsky (Russia)
Type
Published Article
Journal
Russian Aeronautics
Publisher
Pleiades Publishing
Publication Date
Oct 01, 2017
Volume
60
Issue
4
Pages
500–507
Identifiers
DOI: 10.3103/S1068799817040043
Source
Springer Nature
Keywords
License
Yellow

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.

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