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Passive Aeroelastic Tailored Wing Modal Test Using the Fixed Base Correction MethodNo abstract available
Document ID
20200001758
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Spivey, Natalie (NASA Armstrong Flight Research Center Edwards, CA, United States)
Saltzman, Rachel (NASA Armstrong Flight Research Center Edwards, CA, United States)
Wieseman, Carol (NASA Langley Research Center Hampton, VA, United States)
Napolitano, Kevin (ATA Engineering, Inc. San Diego, CA, United States)
Smith, Benjamin (Aurora Flight Sciences Corp. Manassas, VA, United States)
Date Acquired
March 19, 2020
Publication Date
February 10, 2020
Subject Category
Structural Mechanics
Report/Patent Number
AFRC-E-DAA-TN77676
Meeting Information
Meeting: Conference and Exposition on Structural Dynamics: IT’S NOT JUST MODAL ANYMORE
Location: Houston, TX
Country: United States
Start Date: February 10, 2020
End Date: February 13, 2020
Sponsors: Society for Experimental Mechanics, Inc.
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
structural dynamics
modal testing

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