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Aeroelastic Response of the Adaptive Compliant Trailing Edge Transition SectionThis presentation describes an unconventional process for analyzing and validating non-linear aerostructures.
Document ID
20160000699
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Herrera, Claudia Y. (NASA Dryden Flight Research Center Edwards, CA United States)
Spivey, Natalie D. (NASA Dryden Flight Research Center Edwards, CA United States)
Lung, Shun-Fat (Jacobs Engineering Group, Inc. Edwards AFB, CA, United States)
Date Acquired
January 12, 2016
Publication Date
January 4, 2016
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
DFRC-E-DAA-TN28787
Report Number: DFRC-E-DAA-TN28787
Meeting Information
Meeting: AIAA SciTech 2016
Location: San Diego, CA
Country: United States
Start Date: January 4, 2016
End Date: January 8, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NND08RR01B
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
aircraft stability
airworthiness
ground vibration test

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