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Analysis Of Demonstration Low Speed Wind Tunnel Test Data, M-DAW technical Note, WP4 task 4.10

Streit, Thomas and Rohardt, Claas-Hinrik and Hantrais Gervois, Jean-Luc (2006) Analysis Of Demonstration Low Speed Wind Tunnel Test Data, M-DAW technical Note, WP4 task 4.10. DLR-Interner Bericht. IB-125-2006/913.

Full text not available from this repository.

Abstract

Pressure distribution analysis is given for the M-DAW low speed wind tunnel tests with the model XO3D1. Low speeds were performed in the KKK-DNW (July 2003) with the reference tip devices and in the ETW (November 2005) using the novel downward pointed winglet and the Küchemann tip. For the low speed ETW take-off configuration tests, results are compared between the downward pointing winglet and the reference Küchemann tip device. In addition, ETW and DNW-KKK test results for the take-off configuration with Küchemann tip are compared. ETW low speed test results for the clean X03D1 with the downward pointing winglet are compared to (Elsa) Navier-Stokes results obtained by ONERA using the N-47 configuration

Item URL in elib:https://elib.dlr.de/46775/
Document Type:Monograph (DLR-Interner Bericht)
Additional Information:M-DAW Technical Note, Reference MDAW-DLR-410-N009
Title:Analysis Of Demonstration Low Speed Wind Tunnel Test Data, M-DAW technical Note, WP4 task 4.10
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Streit, ThomasUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Rohardt, Claas-HinrikUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Hantrais Gervois, Jean-LucAplied Aerodynamics Department, ONERAUNSPECIFIEDUNSPECIFIED
Date:July 2006
Refereed publication:No
Open Access:No
Status:Published
Keywords:ETW, DNW-KKK, low speed test, Küchemann tip, downward pointing winglet, Navier Stokes
HGF - Research field:Aeronautics, Space and Transport (old)
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: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Configuration Design
Deposited By: Streit, Dr.rer.nat. Thomas
Deposited On:11 Jan 2007
Last Modified:27 Apr 2009 13:24

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