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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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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.

Item URL in elib:https://elib.dlr.de/36331/
Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=1995,
Title:ALVAST Half-Model Investigations in the Low-Speed Wind Tunnel Braunschweig
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Open Access:No
Number of Pages:75
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 (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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