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Higher-order flow angle corrections for three-dimensional wind tunnel wall interferenceA second-order theory including camber effects in wind tunnel wall interference corrections is described. Changes in the geometrical configuration of the model tested are avoided by introducing the camber correction as an equivalent angle-of-attack correction. Tabular and graphic data are presented which indicate improved accuracy for second-order over first-order theory.
Document ID
19820060711
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Rizk, M. H.
(Flow Research Co. Kent, WA, United States)
Date Acquired
August 10, 2013
Publication Date
October 1, 1982
Publication Information
Publication: Journal of Aircraft
Volume: 19
Subject Category
Research And Support Facilities (Air)
Accession Number
82A44246
Funding Number(s)
CONTRACT_GRANT: NAS1-16262
Distribution Limits
Public
Copyright
Other

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