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Wind Tunnel Investigation of the A320 Laminar Fin

Schmitt, V.* and Quast, A. and Hinsinger**, (1996) Wind Tunnel Investigation of the A320 Laminar Fin. In: Proc. Second Laminar Flow Forum, 10.-12.6.1996, Bordeaux..

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Among the most ambitious and also advanced european projects dealing with the hybrid laminar flow technology figures the A320 laminar fin programme which has been initiated some years ago by Airbus Industrie in close cooperation with ONERA and DLR. A very important step in this programme which is now in its final phase devoted to the evaluation of the concept by flight tests, was the previous one aiming at the wind tunnel demonstration. The achievement of this phase was based on tests in the ONERA S1MA wind tunnel with a 1/2 scale model of the A320 fin equipped with a suction system into the leading edge and an ALT-avoidance device on the leading edge near the root. With this model, which has been provided by DLR, it was possible to carry out tests in S1MA at cruise conditions with inflight Reynolds numbers. The wind tunnel investigation comprised two separate test campaigns. The first test took place in January 1993. It demonstrated the.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1996, pages=10,
Title:Wind Tunnel Investigation of the A320 Laminar Fin
AuthorsInstitution or Email of Authors
Hinsinger**, UNSPECIFIED
Journal or Publication Title:Proc. Second Laminar Flow Forum, 10.-12.6.1996, Bordeaux.
HGF - Research field:UNSPECIFIED
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):L - Concepts & Integration
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik
Deposited By: elib DLR-Beauftragter
Deposited On:03 Apr 2006
Last Modified:27 Apr 2009 10:06

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