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Residual Strength Prediction of Damaged Aircraft Structure Using 3D Finite Element Modeling and Response Surface Methodology
Document ID
20200003253
Acquisition Source
Langley Research Center
Document Type
Poster
Authors
A D Spear
(Cornell University Ithaca, United States)
A R Ingraffea
(Cornell University Ithaca, United States)
Edward H Glaessgen
(Langley Research Center Hampton, United States)
Date Acquired
May 7, 2020
Subject Category
Structural Mechanics
Report/Patent Number
Report Number: NF1676L-9825
NF1676L-9825
Meeting Information
Meeting: NASA Aviation Safety Technical Conference
Location: McLean, VA
Country: US
Start Date: November 17, 2009
End Date: November 19, 2009
Sponsors: National Aeronautics and Space Administration
Funding Number(s)
WBS: 645846.02.07.07.12.03
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
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