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Re-Effect on MiniTED Performance in High Speed: Validation and Prediction

Richter, Kai (2005) Re-Effect on MiniTED Performance in High Speed: Validation and Prediction. AWIATOR Technical Workshop, 2005-11-05, Bremen.

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Abstract

Within the EU-platform AWIATOR a numerical simulation on the aerodynamic effect of MiniTEDs on an Airbus A340-300 has been conducted at wind-tunnel and free-flight conditions for cruise-flight Mach number and lift coefficients. Therefor, a baseline aircraft cruise configuration and a cruise configuration with MiniTEDs applied to the wing trailing-edge have been simulated with the DLR TAU code. The MiniTEDs have been realised by the use of Split Flaps. The results show a good qualitative agreement with wind-tunnel experiments in terms of lift and drag, the MiniTED influence on the drag polar has been reproduced properly. Comparisons of wing-surface pressure-distributions show a good agreement with the experimental data in all wing sections and prove the MiniTED influence on the aerodynamic coefficients. At free-flight conditions the MiniTED influence is seen to increase compared to the wind-tunnel conditions. Here, the lift-enhancing effect increases and the drag differences compared to the baseline configuration are affected unfavourably. The minimum lift coefficient of profitable MiniTED use is shifted to higher lift. Remaining drag reductions at high lift coefficients diminish. The pressure distributions prove the altered MiniTED influence in detail and show that the deflection angle of the MiniTEDs is too high for free-flight conditions. An additional comparison of numerical and flight-test pressure distributions of the baseline configuration shows a good overall agreement when the in-flight wing-twist is being considered.

Item URL in elib:https://elib.dlr.de/21992/
Document Type:Conference or Workshop Item (Speech)
Title:Re-Effect on MiniTED Performance in High Speed: Validation and Prediction
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Richter, KaiUNSPECIFIEDUNSPECIFIED
Date:5 November 2005
Refereed publication:No
Open Access:No
In DOAJ:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:AWIATOR, Airbus A340, MiniTED, cruise flight, wind tunnel test, free flight test, Reynolds number effect, Split Flap, TAU code, lift enhancement, drag reduction
Event Title:AWIATOR Technical Workshop
Event Location:Bremen
Event Type:Other
Event Dates:2005-11-05
Organizer:Airbus Deutschland GmbH
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics (old)
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > High Speed Configurations
Deposited By: Richter, Kai
Deposited On:30 Jan 2006
Last Modified:27 Apr 2009 04:57

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