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Validation of computational aeroelasticityThe topics are presented in viewgraph form and include the following: codes for computational aeroelasticity validation; the benchmark transonic flutter (BTF) model; BTF testing; the BTF model program; features of transonic flutter; characteristics of attached and separated flow for complete aircraft; and the benchmark aeroelastic model program.
Document ID
19920075810
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Whitlow, Woodrow, Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1987
Publication Information
Publication: NASA. Ames Research Center, NASA CFD Validation Workshop
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
92N70934
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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