van der Wall, Berend G. (2018) Estimate of Rotor Controls and Blade Flapping Caused by an Orthogonal Vortex Disturbance. Journal of the American Helicopter Society, 63 (2), pp. 1-6. American Helicopter Society. doi: 10.4050/JAHS.63.025001. ISSN 0002-8711.
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Abstract
Based on blade element/momentum theory the aerodynamic impact on rotor controls and blade flapping caused by a straight line vortex penetrating orthogonally the plane of a rotor disk is solved using a realistic swirl velocity profile. The collective and cyclic controls needed for disturbance rejection and the coning and cyclic flapping motion developing are computed.
Item URL in elib: | https://elib.dlr.de/113672/ | ||||||||
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Document Type: | Article | ||||||||
Title: | Estimate of Rotor Controls and Blade Flapping Caused by an Orthogonal Vortex Disturbance | ||||||||
Authors: |
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Date: | April 2018 | ||||||||
Journal or Publication Title: | Journal of the American Helicopter Society | ||||||||
Refereed publication: | Yes | ||||||||
Open Access: | No | ||||||||
Gold Open Access: | No | ||||||||
In SCOPUS: | Yes | ||||||||
In ISI Web of Science: | Yes | ||||||||
Volume: | 63 | ||||||||
DOI: | 10.4050/JAHS.63.025001 | ||||||||
Page Range: | pp. 1-6 | ||||||||
Publisher: | American Helicopter Society | ||||||||
ISSN: | 0002-8711 | ||||||||
Status: | Published | ||||||||
Keywords: | Wake vortex interaction, helicotper trim, rotor blade motion | ||||||||
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: | 15 Feb 2018 15:12 | ||||||||
Last Modified: | 30 Oct 2023 14:47 |
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