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Compressibility Effects in Rotorcraft Applications

Pahlke, Klausdieter G. (2010) Compressibility Effects in Rotorcraft Applications. In: John Wiley & Sons, Ltd Encyclopdia of Aerospace Engineering. John Wiley & Sons, Ltd.. pp. 337-342. ISBN 978-0-470-075440-5.

Full text not available from this repository.

Abstract

Compressibility effects play an important role in rotorcraft applications. They limit the high speed performance of rotorcraft because of wave drag and they are the reason for the emission of high speed impulsive noise. Furthermore compressibility triggers flow separation on highly loaded rotors in forward flight (dynamic stall).

Item URL in elib:https://elib.dlr.de/68886/
Document Type:Book Section
Title:Compressibility Effects in Rotorcraft Applications
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Pahlke, Klausdieter G.DLRUNSPECIFIED
Date:27 October 2010
Journal or Publication Title:John Wiley & Sons, Ltd
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 337-342
Editors:
EditorsEmail
Blockley, R.UNSPECIFIED
Shyy, W.UNSPECIFIED
Publisher:John Wiley & Sons, Ltd.
Series Name:Encyclopdia of Aerospace Engineering
ISBN:978-0-470-075440-5
Status:Published
Keywords:Compressibility, rotorcraft, performance, high speed impulsive noise, dynamic stall.
HGF - Research field:Aeronautics, Space and Transport (old), Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics, Aeronautics
HGF - Program Themes:Rotorcraft (old), Rotorcraft (old)
DLR - Research area:Aeronautics, Aeronautics
DLR - Program:L RR - Rotorcraft Research, L RR - Rotorcraft Research
DLR - Research theme (Project):L - The Virtual Aerodynamic Rotorcraft (old), L - The Quiet and Comfortable Rotorcraft (old)
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Helicopters
Deposited By: Pahlke, Dr.-Ing. Klausdieter
Deposited On:24 May 2011 11:35
Last Modified:24 May 2011 11:35

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