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Model deformation measurements in DNW-NWB within the DLR project ForMEx

Kirmse, Tania (2007) Model deformation measurements in DNW-NWB within the DLR project ForMEx. ODAS 2007 – 8th ONERA-DLR Aerospace Symposium, 2007-10-17 - 2007-10-19, Göttingen, Germany.

Full text not available from this repository.

Abstract

Within the DLR Project ForMEx, a model deformation measurement was performed in the low speed wind tunnel DNW - NWB by means of the Image Pattern Correlation Technique (IPCT). The deformation of the F11-half model with a span of 1.4 m was measured in its landing configuration, thusso that the deformation measurement includes not only the determination of the bend and the twist of the main wing, but also the measurement of the gap variation between the main wing and(?)of the slat orand the flap. The wind tunnel runs were performed at Mach 0.2 at several angles of attack, especially in the region of the maximum lift coefficient.

Item URL in elib:https://elib.dlr.de/47877/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Model deformation measurements in DNW-NWB within the DLR project ForMEx
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Kirmse, TaniaUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:2007
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:CD-ROM
Page Range:pp. 1-14
Series Name:Conference Proceedings
Status:Published
Keywords:model deformation measurement, Image Pattern Correlation Technique (IPCT)
Event Title:ODAS 2007 – 8th ONERA-DLR Aerospace Symposium
Event Location:Göttingen, Germany
Event Type:international Conference
Event Start Date:17 October 2007
Event End Date:19 October 2007
Organizer:DLR/ONERA
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics (old)
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Experimental Methods
Deposited By: Micknaus, Ilka
Deposited On:13 Nov 2007
Last Modified:24 Apr 2024 19:10

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