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ALVAST Half-Model Investigations in the Low-Speed Wind Tunnel Braunschweig

Puffert-Meissner, W. (1995) ALVAST Half-Model Investigations in the Low-Speed Wind Tunnel Braunschweig. DLR-Interner Bericht. 129-95/11, 75 S.

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Abstract

The ALVAST half-model was investigated with a high-lift wing without engine simulator in the DNW/NWB Low-Speed Wind Tunnel Braunschweig in June 1994 at the Mach numbers 0.12, 0.18 and 0.22 in order to check this configuration for the first time in a wind tunnel and to investigate the half-model test technique in this wind tunnel. The model geometry and the model mounting in the test section are described. Results of the force and pressure distribution measurements are analyzed and the improvements of the high-lift capabilities achieved by a number of modifications are discussed and presented.

Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=1995,
Title:ALVAST Half-Model Investigations in the Low-Speed Wind Tunnel Braunschweig
Authors:
AuthorsInstitution or Email of Authors
Puffert-Meissner, W.UNSPECIFIED
Date:1995
Number of Pages:75
Status:Published
Keywords:Half-Model, low-speed, high-lift, wind tunnel test technique
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 10:05

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