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Wind Tunnel Report TN2621: Static Force, Moment, Surface Pressure and PSP Measurements on the DLR-F19 Con-figuration including Spoiler Geometries and Control Surfaces

Huber, Kerstin Claudie and Henne, Ulrich and Löser, Thomas and Schütte, Andreas (2017) Wind Tunnel Report TN2621: Static Force, Moment, Surface Pressure and PSP Measurements on the DLR-F19 Con-figuration including Spoiler Geometries and Control Surfaces. Other. DLR-Interner Bericht. EB 124-2017/901, 180 S.

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Abstract

In order to assess the influence of various spoiler geometries on the low-speed aerodynamic properties and the flight mechanical behavior of the DLR-F19 configuration, static forces, moments and surface pressure measurements have been conducted in the Low SpeedWind Tunnel Facility (NWB) of the Dutch-German Wind Tunnels (DNW) in Braunschweig. Further, first time Pressure Sensitive Paint (PSP) measurements on the undeflected and deflected trailing edge control surfaces of the DLRF19 have been performed. These test have been conducted within the DLR internal project Mephisto (Milit¨arische Forschung zu Verfahren und Technologien f ¨ ur den Gesamtentwurf von UAVs). This test campaign is the third wind tunnel test campaign with the DLR-F19 within the DNW-NWB.

Item URL in elib:https://elib.dlr.de/110803/
Document Type:Monograph (DLR-Interner Bericht, Other)
Title:Wind Tunnel Report TN2621: Static Force, Moment, Surface Pressure and PSP Measurements on the DLR-F19 Con-figuration including Spoiler Geometries and Control Surfaces
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Huber, Kerstin ClaudieKerstin.Huber (at) dlr.deUNSPECIFIED
Henne, Ulrichulrich.henne (at) dlr.deUNSPECIFIED
Löser, Thomasthomas.loeser (at) dnw.aeroUNSPECIFIED
Schütte, AndreasAndreas.Schuette (at) dlr.deUNSPECIFIED
Date:January 2017
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:180
Status:Published
Keywords:Mephisto, UCAV, control surfaces, vortical flow, Partical Image Velocimetry, PSP, Experiment
Institution:DLR
Department:Institut für Aerodynamik und Strömungstechnik
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 - Military Technologies
Location: Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Transport Aircraft
Institute of Aerodynamics and Flow Technology > Experimental Methods
German-Dutch Windtunnels
Deposited By: Schütte, Andreas
Deposited On:24 Jan 2017 13:39
Last Modified:24 Jan 2017 13:39

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