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AGARD Standard Aeroelastic Configurations for Dynamic Response I - Wing 445.6This report contains experimental flutter data for the AGARD 3D swept tapered standard configuration "Wing 445.6", along with related descriptive data of the model properties required for comparative flutter calculations. As part of a cooperative AGARD-SMP programme, guided by the Sub-Committee on Aeroelasticity, this standard configuration may serve as a common basis for comparisons of calculated and measured aeroelastic behaviour. These comparisons will promote a better understanding of the assumptions, approximations and limitations underlying the various aerodynamic methods applied, thus pointing the way to further improvements.
Document ID
19880017809
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
E. Carson Yates, Jr.
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
September 5, 2013
Publication Date
July 1, 1988
Publication Information
Publisher: Advisory Group for Aerospace Research and Development
ISBN: 92-835-0463-1
Subject Category
Aerodynamics
Report/Patent Number
AGARD-R-765
AD-A199433
Meeting Information
Meeting: 61st Meeting of the Structures and Materials Panel
Location: Oberammergau
Country: DE
Start Date: September 8, 1985
End Date: September 13, 1985
Sponsors: North Atlantic Treaty Organization
Accession Number
88N27193
Distribution Limits
Public
Copyright
Other
Keywords
Aircraft
Aeroelasticity
Aerodynamics
Transonic flow
Methodology
Experimental data
Predictions
Models
Dynamic response
Configurations
Numerical methods and procedures
Fluid dynamics
Flutter
Swept wings
Taper
Aerodynamic configurations
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