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.
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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.
|Document Type:||Monograph (DLR-Interner Bericht)|
|Title:||Load test on the ALVAST High-Lift Wing|
|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:||L - no assignement|
|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 10:05|
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