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Instrumentation, techniques and data reduction associated with airfoil testing programs at Wichita State UniversityTwo dimensional airfoil testing was conducted at the Wichita State University Beech Wind Tunnel for a number of years. The instrumentation developed and adapted during this period of testing for determination of flow fields along with traversing mechanisms for these probes are discussed. In addition, some of the techniques used to account for interference effects associated with the apparatus used for this two dimensional testing are presented. The application of a minicomputer to the data reduction and presentation is discussed.
Document ID
19790011825
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rodgers, E. J.
(Wichita State Univ. Wichita, KS, United States)
Wentz, W. H., Jr.
(Wichita State Univ. Wichita, KS, United States)
Seetharam, H. C.
(Boeing Commercial Airplane Co.)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Publication Information
Publication: NASA. Langley Res. Center Advanced Technol. Airfoil Res., Vol. 1, Pt. 2
Subject Category
Instrumentation And Photography
Accession Number
79N19996
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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