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

A. A. Aparinov; B. S. Kritskii; A. V. Setukha

doi:10.3103/S1068799817040043

Access to the full text

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.

Report this publication

Statistics

Seen <100 times