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
04.01.2016
Sonstige
Keine Angabe
Englisch
British Library Conference Proceedings | 2016
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