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.

Abstract

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

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD
Kiock, R.	UNSPECIFIED	UNSPECIFIED

Date:

1994

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Number of Pages:

Status:

Published

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

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