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Stall Effects and Blade Torsion - An Evaluation of Predictive Tools

Petot, Didier and Arnaud, Gilles and Harrison, Robert and Stevens, Jos and Dieterich, Oliver and van der Wall, Berend G. and Young, Colin and Széchényi, E. (1999) Stall Effects and Blade Torsion - An Evaluation of Predictive Tools. Journal of the American Helicopter Society, 44 (4), pp. 320-332. American Helicopter Society International. doi: 10.1999.

Full text not available from this repository.

Abstract

The various comprehensive codes of the participating organizations are used for computation of rotor experiments close to and within stall. Special emphasis is made to the prediciton of dynamic stall in lift and moment and the dynamic response of the rotor blade. Comparison of rotor power computed and experimentally evaluated is performed.

Item URL in elib:https://elib.dlr.de/60454/
Document Type:Article
Title:Stall Effects and Blade Torsion - An Evaluation of Predictive Tools
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Petot, DidierOneraUNSPECIFIEDUNSPECIFIED
Arnaud, GillesECUNSPECIFIEDUNSPECIFIED
Harrison, RobertWHLUNSPECIFIEDUNSPECIFIED
Stevens, JosNLRUNSPECIFIEDUNSPECIFIED
Dieterich, OliverECDUNSPECIFIEDUNSPECIFIED
van der Wall, Berend G.DLRUNSPECIFIEDUNSPECIFIED
Young, ColinDERAUNSPECIFIEDUNSPECIFIED
Széchényi, E.OneraUNSPECIFIEDUNSPECIFIED
Date:October 1999
Journal or Publication Title:Journal of the American Helicopter Society
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:Yes
Volume:44
DOI:10.1999
Page Range:pp. 320-332
Publisher:American Helicopter Society International
Status:Published
Keywords:GARTEUR, rotor blade stall, elastic torsion
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Rotorcraft (old)
DLR - Research area:Aeronautics
DLR - Program:L RR - Rotorcraft Research
DLR - Research theme (Project):L - The Active Rotorcraft (old)
Location: Braunschweig
Institutes and Institutions:Institute of Flight Systems > Rotorcraft
Deposited By: van der Wall, Prof. Dr. Berend G.
Deposited On:28 Oct 2009 10:57
Last Modified:28 Oct 2009 10:57

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