Comparative Study of Coaxial Main Rotor Aerodynamics at Forward Flight Based on Free Wake Model and Unsteady ReynoldsAveraged Navier

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Comparative Study of Coaxial Main Rotor Aerodynamics at Forward Flight Based on Free Wake Model and Unsteady ReynoldsAveraged Navier–Stokes Method

Published:2022 Issue: Volume:14 Page:
ISSN:2175-9146
Container-title:Journal of Aerospace Technology and Management
language:
Short-container-title:J. Aerosp. Technol. Manag.

Author:

Konstantinov Sergey Gennadievich¹^ORCID,Ignatkin Yuri Mikhailovich¹^ORCID,Makeev Pavel Viacheslavovich¹^ORCID,Shomov Alexander Ivanovich¹^ORCID,Nikitin Sergey Olegovich¹^ORCID

Affiliation:

1. Moscow Aviation Institute, Russian Federation

Publisher

FapUNIFESP (SciELO)

Subject

Aerospace Engineering

Link

http://www.scielo.br/pdf/jatm/v14/2175-9146-jatm-14-e0822.pdf

Reference28 articles.

1. Flight Investigation of Coaxial Rotor Tip Vortex Structure. Paper presented AHS 50th Annual Forum;Akimov AI,1994

2. Mathematical modeling of Ka-226 / Ka-26 helicopter main rotor blade flapping motion at rotor acceleration / deceleration in wind conditions;Bourtsev BN,2007

3. Paper presented 27rd European Rotorcraft Forum;Bourtsev BN,2001

4. Aerodynamic characteristics of rigid coaxial rotor by wind tunnel test and numerical calculation;Deng J;Chinese J Aeronaut,2019

5. A Hybrid CFD Method for Coaxial Rotor Performance Prediction in Forward Flight, Paper presented AHS Aeromechanics Specialists Conference on Aeromechanics;Egolf TA,2010

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Analysis of Rotor Tip Vortex Circulation in the Near Field;Russian Aeronautics;2023-12

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