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Steady Aerodynamics of Miniature Trailing-Edge Devices in Transonic Flows

Richter, Kai and Rosemann, Henning (2011) Steady Aerodynamics of Miniature Trailing-Edge Devices in Transonic Flows. 29th AIAA Applied Aerodynamics Conference, 27. - 30. Juni 2011, Honolulu, Hawaii, USA.

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Official URL: http://www.aia.org

Abstract

The paper describes results of a comprehensive experimental and numerical investigation of the aerodynamics of miniature trailing-edge devices (MiniTEDs) on a supercritical airfoil at transonic speeds. The influence of MiniTEDs on the two-dimensional airfoil flow and on the aerodynamic coefficients is presented in detail for the Gurney flap, the split flap and the divergent trailing-edge. The influence of geometry parameters is discussed for the Gurney flap height, the split flap deflection angle and the MiniTED position, as well as for different types of perforation. The use of MiniTEDs as adaptive elements is presented for drag-optimal operation and is compared to the performance of a flexible trailing-edge. The influence of different freestream parameters is discussed for the Mach number and the Reynolds number.

Document Type:Conference or Workshop Item (Speech, Paper)
Title:Steady Aerodynamics of Miniature Trailing-Edge Devices in Transonic Flows
Authors:
AuthorsInstitution or Email of Authors
Richter, KaiUNSPECIFIED
Rosemann, HenningUNSPECIFIED
Date:27 June 2011
Refereed publication:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 1-19
Series Name:Conference Proceedings
Status:Published
Keywords:MiniTEDs, Gurney flap, split flap, divergent trailing-edge, flexible trailing-edge, airfoil flow, wind tunnel experiment, numerical simulation, flow control
Event Title:29th AIAA Applied Aerodynamics Conference
Event Location:Honolulu, Hawaii, USA
Event Type:international Conference
Event Dates:27. - 30. Juni 2011
Organizer:American Institute of Aeronautics and Astronautics
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Helicopters
Institute of Aerodynamics and Flow Technology > High Speed Configurations
Deposited By: Kai Richter
Deposited On:19 Aug 2011 08:20
Last Modified:19 Aug 2011 08:20

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