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Analytical Estimate of Rotor Controls Required for a Propeller Wake Disturbance Rejection

van der Wall, Berend G. (2024) Analytical Estimate of Rotor Controls Required for a Propeller Wake Disturbance Rejection. Journal of the American Helicopter Society, 69, pp. 1-6. American Helicopter Society. doi: 10.4050/JAHS.69.045011. ISSN 0002-8711.

Full text not available from this repository.

Abstract

During helicopter air-to-air refueling, the aircraft propeller’s jet can engage with the helicopter rotor. The impact on the helicopter rotor thrust and aerodynamic hub moments is solved analytically for the first time, based on blade element momentum theory. The collective and cyclic blade pitch controls needed for disturbance rejection are computed for a typical air-to-air refueling scenario. A propeller jet affecting the retreating side of the rotor requires much more pilot controls to retrim than an impingement on the advancing side.

Item URL in elib:https://elib.dlr.de/201260/
Document Type:Article
Additional Information:Arbeiten wurden im Rahmen des DLR Projektes URBAN-Rescue durchgeführt.
Title:Analytical Estimate of Rotor Controls Required for a Propeller Wake Disturbance Rejection
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
van der Wall, Berend G.UNSPECIFIEDhttps://orcid.org/0000-0001-6144-0921165906423
Date:2024
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:69
DOI:10.4050/JAHS.69.045011
Page Range:pp. 1-6
Publisher:American Helicopter Society
ISSN:0002-8711
Status:Published
Keywords:Helicopter, interactional aerodynamcis, Propeller-rotor interaction, blade element momentum theory
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Efficient Vehicle
DLR - Research area:Aeronautics
DLR - Program:L EV - Efficient Vehicle
DLR - Research theme (Project):L - Virtual Rotorcraft and Validation
Location: Braunschweig
Institutes and Institutions:Institute of Flight Systems > Rotorcraft
Institute of Flight Systems
Deposited By: van der Wall, Prof. Dr. Berend G.
Deposited On:21 Aug 2024 14:22
Last Modified:21 Aug 2024 14:22

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