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Effect of Vortex Deflection on Vortex-Rotor Interference and Rotor Trim

van der Wall, Berend G. (2021) Effect of Vortex Deflection on Vortex-Rotor Interference and Rotor Trim. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design New Results in Numerical and Experimental Fluid Mechanics XIII, 151. Springer. pp. 407-417. doi: 10.1007/978-3-030-79561-0_39. ISBN 978-3-030-79560-3. ISSN 1612-2909.

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Official URL: https://www.springer.com/gp/book/9783030795603

Abstract

The flight of a helicopter within the wake of a preceding fixed-wing aircraft, for example during air-to-air refueling, is accompanied by vortex-rotor interactions. The full mutuality of vortex and rotor wake interactions requires a free-wake solution that is applied at different advance ratios in this paper and compared to existing simplified models. The results indicate that the simplified models are valid for higher advance ratios whereas very small advance ratios require the use of a free-wake approach.

Item URL in elib:https://elib.dlr.de/136332/
Document Type:Book Section
Title:Effect of Vortex Deflection on Vortex-Rotor Interference and Rotor Trim
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
van der Wall, Berend G.UNSPECIFIEDhttps://orcid.org/0000-0001-6144-0921148018652
Date:13 July 2021
Journal or Publication Title:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:151
DOI:10.1007/978-3-030-79561-0_39
Page Range:pp. 407-417
Publisher:Springer
Series Name:New Results in Numerical and Experimental Fluid Mechanics XIII
ISSN:1612-2909
ISBN:978-3-030-79560-3
Status:Published
Keywords:helicopter, helicopter aerodynamics, helicopter safety, aerodynamic interaction, vortex-rotor interaction, rotor trim
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:rotorcraft
DLR - Research area:Aeronautics
DLR - Program:L RR - Rotorcraft Research
DLR - Research theme (Project):L - The Innovative Rotorcraft (old)
Location: Braunschweig
Institutes and Institutions:Institute of Flight Systems > Rotorcraft
Deposited By: van der Wall, Prof. Dr. Berend G.
Deposited On:03 Dec 2021 18:55
Last Modified:04 Dec 2023 12:36

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