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Comparison of Force and Moment Coefficients for the Same Test Article in Multiple Wind TunnelsThis paper compares the results of force and moment measurements made on the same test article and with the same balance in three transonic wind tunnels. Comparisons are made for the same combination of Reynolds number, Mach number, sideslip angle, control surface configuration, and angle of attack range. Between-tunnel force and moment differences are quantified. An analysis of variance was performed at four unique sites in the design space to assess the statistical significance of between-tunnel variation and any interaction with angle of attack. Tunnel to tunnel differences too large to attribute to random error were detected were observed for all forces and moments. In some cases these differences were independent of angle of attack and in other cases they changed with angle of attack.
Document ID
20140000504
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Deloach, Richard
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
January 31, 2014
Publication Date
June 24, 2013
Subject Category
Aerodynamics
Report/Patent Number
NF1676L-16794
Report Number: NF1676L-16794
Meeting Information
Meeting: AIAA Ground Testing Conference
Location: San Diego, CA
Country: United States
Start Date: June 24, 2013
End Date: June 27, 2013
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 425425.01.02.07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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