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Transonic Wind Tunnel Measurements of Double- and Triple-Delta Wing Configurations

Rein, Martin and Henne, Ulrich and Yorita, Daisuke and Hövelmann, Andreas and Lohmann, Rick (2019) Transonic Wind Tunnel Measurements of Double- and Triple-Delta Wing Configurations. DLR-Interner Bericht. DLR-IB-AS-GO-2018-79, 61 S.

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Abstract

Results are reported of three wind tunnel campaigns performed in the transonic wind tunnels DNW-TWG and DNW-HST. The NA2 multi-delta wing model was tested with two triple- and one double-delta wing planform. The corresponding configurations are known as NA2-W1, NA2-W2 and NA2-W3. Tests were performed without control surfaces and also with deflected LEVCONS and leading edge slats. The model was tested at Mach numbers in the range M = 0.4 - 1.3 with a focus on M = 0.50, 0.85 and 1.10. The corresponding Reynolds number range was Re = 7.7-106 - 13.3-10s. A focus was on high angle of attack aerodynamics with angles of attack up to 40°. For all configurations angle of attack sweeps were performed at different angles of sideslip, and sweeps of the angle of sideslip (-10° < ß < 10°) at different angles of attack. In addition, for selected flow conditions pressure distributions were determined on the lee side of the NA2-W1 configuration by means of pressure sensitive paint. A complete compilation of all tests is provided and results are briefly reviewed and exemplarily discussed.

Item URL in elib:https://elib.dlr.de/133345/
Document Type:Monograph (DLR-Interner Bericht)
Title:Transonic Wind Tunnel Measurements of Double- and Triple-Delta Wing Configurations
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Rein, Martinmartin.rein (at) dlr.dehttps://orcid.org/0000-0002-2670-2815
Henne, Ulrichulrich.henne (at) dlr.deUNSPECIFIED
Yorita, Daisukedaisuke.yorita (at) dlr.deUNSPECIFIED
Hövelmann, AndreasAirbus Defence & Space GmbHUNSPECIFIED
Lohmann, RickAirbus Defence & Space GmbHUNSPECIFIED
Date:December 2019
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:61
Status:Published
Keywords:delta wing, double delta wing, transonic flow, wind tunnel test
Institution:AS
Department:HGK
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: Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > High Speed Configurations, GO
Institute for Aerodynamics and Flow Technology > Experimental Methods, GO
Deposited By: Rein, Prof.Dr. Martin
Deposited On:08 Jan 2020 16:04
Last Modified:08 Jan 2020 16:04

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