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Airfoils with Dynamic Transonic Flow Control

Trenker, M. and Geißler, W. and Sobieczky, M. (2000) Airfoils with Dynamic Transonic Flow Control. 18th AIAA Applied Aerodynamics Conference & Exhibit, Denver, CO, 14-17 Aug.2000.

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Abstract

Design modifications to airfoils in unsteady transonic flow are carried out by means of realistic geometry modeling and systematic transonic design removal of recompression shocks. Results of systematic design lead to simplified shape modification functions shortcutting the use of 2D steady and unsteady numerical methods and help extending design knowledge base to improving airfoils for helicopter rotors and dynamic stall control.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2001,
Title:Airfoils with Dynamic Transonic Flow Control
Authors:
AuthorsInstitution or Email of Authors
Trenker, M.UNSPECIFIED
Geißler, W.UNSPECIFIED
Sobieczky, M.UNSPECIFIED
Date:2000
Status:Published
Keywords:Dynamic Stall, transonic, aerodynamics, design, Flow control, unsteady
Event Title:18th AIAA Applied Aerodynamics Conference & Exhibit, Denver, CO, 14-17 Aug.2000
Organizer:AIAA, 2000 -4419
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Rotorcraft
DLR - Research area:Aeronautics
DLR - Program:L RR - Rotorcraft Research
DLR - Research theme (Project):UNSPECIFIED
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Strömungsmechanik
Deposited By: elib DLR-Beauftragter
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 20:58

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