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New Flutter Analysis Technique for Time-Domain Computational AeroelasticityThis presentation is a conference companion and discusses a new flutter analysis technique using CFD results.
Document ID
20170000462
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Pak, Chan-Gi (NASA Armstrong Flight Research Center Edwards, CA United States)
Lung, Shun-Fat (Jacobs Technology, Inc. Edwards AFB, CA, United States)
Date Acquired
January 18, 2017
Publication Date
January 9, 2017
Subject Category
Fluid Mechanics And Thermodynamics
Aircraft Stability And Control
Report/Patent Number
DFRC-E-DAA-TN37810
Report Number: DFRC-E-DAA-TN37810
Meeting Information
Meeting: AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
Location: Grapevine, TX
Country: United States
Start Date: January 9, 2017
End Date: January 13, 2017
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NND08RR01B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HWB aircraft
flutter analysis
aeroelasticity

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