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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.
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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/ | ||||||
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| Document Type: | Book Section | ||||||
| Title: | Compressibility Effects in Rotorcraft Applications | ||||||
| Authors: |
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| 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: |
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| 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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