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PAT Wing Fixed Base Correction Modal Testing DebriefThis presentation is an overview of the PAT (Passive Aeroelastic Tailored) Wing ground vibration test and the fixed-base correction research being performed here.
Document ID
20180006673
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Napolitano, Kevin (ATA Engineering, Inc. San Diego, CA, United States)
Spivey, Natalie (NASA Armstrong Flight Research Center Edwards, CA, United States)
Miller, Kia (NASA Armstrong Flight Research Center Edwards, CA, United States)
Date Acquired
October 24, 2018
Publication Date
September 6, 2018
Subject Category
Aircraft Design, Testing And Performance
Structural Mechanics
Report/Patent Number
AFRC-E-DAA-TN60636
Report Number: AFRC-E-DAA-TN60636
Meeting Information
Meeting: NESC Meeting Debrief
Location: WebEx online
Country: United States
Start Date: September 6, 2018
Sponsors: NASA Headquarters
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
ground testing

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