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AGARD standard aeroelastic configurations for dynamic responseSince emphasis is on the transonic speed range, special importance is placed on configurations for which available data are sufficient to define accurately a transonic flutter boundary. Only configurations with clean, smooth surfaces are considered suitable. Segmented models or models with surface-slope discontinuities are inappropriate. Excluded also, in general, are configurations and data sets that involve behavior that is uncertain or not well understood, uncertain model properties, or know sensitivities to small variations in model properties. In order to assess the suitability of configurations already tested and the associated data for designation as standard, a survey of AGARD member countries was conducted to seek candidates for the prospective set. The results of that survey are given and summarized along with the initial selection of a standard configuration.
Document ID
19890009875
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Yates, E. Carson, Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1989
Publication Information
Publication: Transonic Unsteady Aerodynamics and Aeroelasticity 1987, Part 1
Subject Category
Aerodynamics
Accession Number
89N19246
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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