This presentation is regarding tool validation used for prediction of the GIII wing normal, bending, and torque loads.
Evaluation of Load Analysis Methods for NASA's GIII Adaptive Compliant Trailing Edge Project
AIAA SciTech 2016 ; 2016 ; San Diego, CA, United States
2016-01-04
Miscellaneous
No indication
English
British Library Conference Proceedings | 2016
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