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Advanced Design Approach for a High-lift Wind Tunnel Model Based on Flight Test Data

Bier, Niko and Keye, Stefan and Rohlmann, David (2014) Advanced Design Approach for a High-lift Wind Tunnel Model Based on Flight Test Data. 4th Joint Symposium of DFG FOR 1066 and DLR C²A²S²E on "Simulation of Wing and Nacelle Stall", 01.-02. Dez. 2014, Braunschweig.

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Item URL in elib:https://elib.dlr.de/91855/
Document Type:Conference or Workshop Item (Speech)
Title:Advanced Design Approach for a High-lift Wind Tunnel Model Based on Flight Test Data
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Bier, Nikoniko.bier (at) dlr.deUNSPECIFIED
Keye, Stefanstefan.keye (at) dlr.deUNSPECIFIED
Rohlmann, Daviddavid.rohlmann (at) dlr.deUNSPECIFIED
Date:1 December 2014
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Model Design, Wind Tunnel, Hochauftrieb
Event Title:4th Joint Symposium of DFG FOR 1066 and DLR C²A²S²E on "Simulation of Wing and Nacelle Stall"
Event Location:Braunschweig
Event Type:international Conference
Event Dates:01.-02. Dez. 2014
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation and Validation
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Bier, Niko
Deposited On:22 Jan 2015 14:52
Last Modified:22 Jan 2015 14:52

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