Prediction of transient responses of a folding wing during the morphing process
Author:
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference12 articles.
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4. On an implementation of the Hilber–Hughes–Taylor method in the context of index 3 differential-algebraic equations of multibody dynamics;Negrut;J. Comput. Nonlinear Dyn.,2007
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