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NLR activities in the field of wind tunnel wall interferenceMeasured field data as a boundary condition for calculating the interference flow field were applied. They are divided into two categories. In the first category, the field data must consist of distributions of a single velocity component, and an accurate estimate of the hypothetical free air contribution of the model to this component is required. The differences between measured values and estimated model contributions are attributed to wall interference and they establish the boundary condition. The associated field data measurements are simple, yet the necessary model representation generally is a serious drawback. The second category requires field data which consist of velocity vector distributions at the price of multicomponent measurements, but at the profit that no information at all is required about the model. In solid wall test sections, the price is reduced to virtually zero but the profit remains.
Document ID
19850003716
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Smith, J.
(National Aerospace Lab. Amsterdam, Netherlands)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Publication Information
Publication: NASA. Langley Research Center Wind Tunnel Wall Interference Assessment and Correction, 1983
Subject Category
Aerodynamics
Accession Number
85N12024
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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