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Unsteady Aerodynamic Validation Experiences From the Aeroelastic Prediction WorkshopThe AIAA Aeroelastic Prediction Workshop (AePW) was held in April 2012, bringing together communities of aeroelasticians, computational fluid dynamicists and experimentalists. The extended objective was to assess the state of the art in computational aeroelastic methods as practical tools for the prediction of static and dynamic aeroelastic phenomena. As a step in this process, workshop participants analyzed unsteady aerodynamic and weakly-coupled aeroelastic cases. Forced oscillation and unforced system experiments and computations have been compared for three configurations. This paper emphasizes interpretation of the experimental data, computational results and their comparisons from the perspective of validation of unsteady system predictions. The issues examined in detail are variability introduced by input choices for the computations, post-processing, and static aeroelastic modeling. The final issue addressed is interpreting unsteady information that is present in experimental data that is assumed to be steady, and the resulting consequences on the comparison data sets.
Document ID
20140007352
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Heeg, Jennifer
(NASA Langley Research Center Hampton, VA, United States)
Chawlowski, Pawel
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
June 12, 2014
Publication Date
January 13, 2014
Subject Category
Aerodynamics
Report/Patent Number
AIAA Paper 2014-0203
NF1676L-16688
Report Number: AIAA Paper 2014-0203
Report Number: NF1676L-16688
Meeting Information
Meeting: AIAA Aerospace Sciences Meeting
Location: National Harbor, MD
Country: United States
Start Date: January 13, 2014
End Date: January 17, 2014
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 473452.02.07.04.02.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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