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Report of the panel on dynamics and aeroelasticityModel scaling for flutter analysis is reviewed. Characteristics of the Langley Transonic Dynamics Tunnel (TDT) are described and several features are recommended for inclusion in the National Transonic Facility. Problem areas suggested for the NTF include: Reynolds number effects on control surface unsteady aerodynamics; effects of Reynolds number on buffet onset and loads; transonic unsteady aerodynamics; and Reynolds number effects on flutter characteristics of wing planforms and airfoils.
Document ID
19770020206
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Houbolt, J. (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
77N27150
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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