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Modal Testing of a Flexible Wing On a Dynamically Active Test Fixture Using the Fixed Base Correction MethodNo abstract available
Document ID
20190026507
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Spivey, Natalie (NASA Armstrong Flight Research Center Edwards, CA, United States)
Miller, Kia (NASA Armstrong Flight Research Center Edwards, CA, United States)
Saltzman, Rachel (NASA Armstrong Flight Research Center Edwards, CA, United States)
Napolitano, Kevin (ATA Engineering, Inc. San Diego, CA, United States)
Date Acquired
June 19, 2019
Publication Date
June 10, 2019
Subject Category
Structural Mechanics
Aircraft Design, Testing And Performance
Report/Patent Number
AFRC-E-DAA-TN69193
Meeting Information
Meeting: International Forum on Aeroelasticity and Structural Dynamics (IFASD)
Location: Savannah GA
Country: United States
Start Date: June 10, 2019
End Date: June 13, 2019
Sponsors: American Institute of Aeronautics and Astronautics (AIAA), Boeing Company
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
modal testing

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