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Adaptive wing model for wind channel tests

Campanie, L. F. and Carli, V. and Sachau, D. (2000) Adaptive wing model for wind channel tests. RTO-Symposium on Active Control Technology, Braunschweig, 08.-11. Mai 2000, Research & Technology Organization, (2000).

Full text not available from this repository.

Abstract

The aim of this work is to realize an adaptive wind channel wing model by means of a „structronic“ concept. The desired geometry changes are achieved through the use of the structural flexibility, and no moveable parts are required. The wind channel model presents two active sections: The „bump“ section, on the upper surface of the airfoil, and the adaptive trailing edge. The changes of the airfoil geometry by means of these parts of the model make possible to vary the distribution of the aerodynamic load on the wing. The activation of the bump and of the trailing edge is realized by means of solide state actuators. A sytem of ca. two hundred shape memory alloy actuators is used. The actuators give here also a contribution to the stiffness of the structure. Here the numerical results of the FEM investigations are presented, as well as the experimental results on the prototypes of the adaptive trailing edge and the bump actuators.

Item URL in elib:https://elib.dlr.de/16514/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2001,
Title:Adaptive wing model for wind channel tests
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Campanie, L. F.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Carli, V.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Sachau, D.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:2000
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Event Title:RTO-Symposium on Active Control Technology, Braunschweig, 08.-11. Mai 2000, Research & Technology Organization, (2000)
Organizer:NATO
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):UNSPECIFIED
Location: Braunschweig
Institutes and Institutions:Institute of Composite Structures and Adaptive Systems > Institut für Strukturmechanik
Deposited By: DLR-Beauftragter, elib
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 16:03

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