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Evaluation of Load Analysis Methods for NASA's GIII Adaptive Compliant Trailing Edge ProjectThis presentation is regarding tool validation used for prediction of the GIII wing normal, bending, and torque loads.
Document ID
20160000700
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Cruz, Josue (NASA Armstrong Flight Research Center Edwards, CA, United States)
Miller, Eric J. (NASA Armstrong Flight Research Center Edwards, CA, United States)
Date Acquired
January 12, 2016
Publication Date
January 4, 2016
Subject Category
Aircraft Design, Testing And Performance
Aerodynamics
Report/Patent Number
AFRC-E-DAA-TN28753
Report Number: AFRC-E-DAA-TN28753
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
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Wings Loads
Aerodynamic Loads
Adaptive Compliant Trailing Edge

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