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Comparison of the NASA Common Research Model European Transonic Wind Tunnel Test Data to NASA Test Data (Invited)

Rivers, Melissa and Quest, Juergen and Rudnik, Ralf (2015) Comparison of the NASA Common Research Model European Transonic Wind Tunnel Test Data to NASA Test Data (Invited). SciTech 2015, 05.-09. Jan. 2015, Kissimmee, USA.

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Abstract

Experimental aerodynamic investigations of the NASA Common Research Model have been conducted in the NASA Langley National Transonic Facility, the NASA Ames 11-ft wind tunnel, and the European Transonic Wind Tunnel. In the NASA Ames 11-ft wind tunnel, data have been obtained at only a chord Reynolds number of 5 million for a wing/body/tail = 0 degree incidence configuration. Data have been obtained at chord Reynolds numbers of 5, 19.8 and 30 million for the same configuration in the National Transonic Facility and in the European Transonic Facility. Force and moment, surface pressure, wing bending and twist, and surface flow visualization data were obtained in all three facilities but only the force and moment, surface pressure and wing bending and twist data are presented herein.

Item URL in elib:https://elib.dlr.de/95284/
Document Type:Conference or Workshop Item (Speech)
Additional Information:AIAA-2015-1093
Title:Comparison of the NASA Common Research Model European Transonic Wind Tunnel Test Data to NASA Test Data (Invited)
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Rivers, Melissas.m.rivers (at) nasa.govUNSPECIFIED
Quest, Juergenjq (at) etw.deUNSPECIFIED
Rudnik, Ralfralf.rudnik (at) dlr.deUNSPECIFIED
Date:January 2015
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Experimental aerodynamic investigations
Event Title:SciTech 2015
Event Location:Kissimmee, USA
Event Type:international Conference
Event Dates:05.-09. Jan. 2015
Organizer:AIAA
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 - Flight Physics
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Grant, Claudia
Deposited On:19 Feb 2015 15:12
Last Modified:31 Jul 2019 19:52

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