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Use of laminar flow technologies for supersonic drag reduction - results of FP project SUPERTRAC

Archambaud, Jean-Pierre and Arnal, Daniel and Hein, Stefan and Sousa, Joao and Hanifi, Ardeshir and Godard, Jean-Luc and Krier, Johann Valentin and Donelli, Raffaele (2008) Use of laminar flow technologies for supersonic drag reduction - results of FP project SUPERTRAC. WCCM8, ECCOMAS 2008, 2008-06-30 - 2008-07-04, Venice, Italy.

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Abstract

The present paper deals with the control of the laminar-turbulent transition on a swept wing in supersonic conditions. This study has been carried out as part of the European Project SUPERTRAC (SUPERsonic TRAnsition Control; January 2005, June 2008). Two issues have been addressed with the same model: the first one is the control of the transition due to crossflow (CF) instabilities present on a swept wing, by using Micron-Sized Roughness elements (MSR); the second one is the prevention of the turbulent contamination along the leading edge by means of appropriate Anti-Contamination Devices (ACD). The paper describes the work concerning the numerical approach, the model design, the tests in the ONERA S2MA wind tunnel in Modane and the analysis of the results.

Item URL in elib:https://elib.dlr.de/59903/
Document Type:Conference or Workshop Item (Paper)
Title:Use of laminar flow technologies for supersonic drag reduction - results of FP project SUPERTRAC
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Archambaud, Jean-PierreONERA, ToulouseUNSPECIFIEDUNSPECIFIED
Arnal, DanielONERA, ToulouseUNSPECIFIEDUNSPECIFIED
Hein, StefanUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Sousa, JoaoIST, LisbonUNSPECIFIEDUNSPECIFIED
Hanifi, ArdeshirFOI, StockholmUNSPECIFIEDUNSPECIFIED
Godard, Jean-LucONERA, ToulouseUNSPECIFIEDUNSPECIFIED
Krier, Johann ValentinIBK, NürnbergUNSPECIFIEDUNSPECIFIED
Donelli, RaffaeleCIRA, CapuaUNSPECIFIEDUNSPECIFIED
Date:2008
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:laminar-turbulent transition, flow control, supersonic, swept wing, attachment-line contamination, crossflow, micron-sized roughness, anti-contamination device
Event Title:WCCM8, ECCOMAS 2008
Event Location:Venice, Italy
Event Type:Conference
Event Start Date:30 June 2008
Event End Date:4 July 2008
HGF - Research field:Aeronautics, Space and Transport
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 > Helicopters
Deposited By: Hein, Dr.-Ing. Stefan
Deposited On:22 Sep 2009 15:21
Last Modified:24 Apr 2024 19:24

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