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Report of the panel on theoretical aerodynamicsRequirements for flow quality in the National Transonic Facility are explored. Viscous flow effects of concern to theoreticians are discussed. Experiments outlined for theory validation in the facility include validating high aspect ratio wing-body combination; low aspect ratio moderately swept wing; low aspect ratio highly swept wing; high lift systems on high aspect ration wings; Reynolds number scaling; dynamic shock- boundary layer interaction; and the effect of R and M on dynamic stall.
Document ID
19770020203
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bobbitt, P. J. (NASA Langley Research Center Hampton, VA, United States)
Carter, J. E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1977
Publication Information
Publication: High Reynolds Number Res.
Subject Category
Research And Support Facilities (Air)
Accession Number
77N27147
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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