DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

Load test on the ALVAST High-Lift Wing

Kiock, R. (1994) Load test on the ALVAST High-Lift Wing. DLR-Interner Bericht. 129-94/13. 33 S.

Full text not available from this repository.


The ALVAST wind tunnel model with high-lift wings is used in the "DUPRIN II" Program which is supported by the European Union. the strength of the wing is proved experimentally because of the complexity of structure and material which is carbonfiber-reinforced polymers. The model has a total span of 3.43m and can be equipped with engine simulators. The high-lift wing withstands a load of more than 1.5 times of that of the nominal aerodynamic load. Since the strain gauges remain on the wing, the strain can also be measured during wind tunnel testing and can be compared with this static load test.

Item URL in elib:https://elib.dlr.de/36239/
Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=1994,
Title:Load test on the ALVAST High-Lift Wing
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Number of Pages:33
Keywords:Transport aircraft model wing, carbonfiber-reinforced polymers, static force simulation of lift and thrust
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 (old)
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik
Deposited By: DLR-Beauftragter, elib
Deposited On:03 Apr 2006
Last Modified:27 Apr 2009 10:05

Repository Staff Only: item control page

Help & Contact
electronic library is running on EPrints 3.3.12
Website and database design: Copyright © German Aerospace Center (DLR). All rights reserved.