Beståndsuppgifter: Reduced uncertainties in the flutter analysis of the aerostructures test wing / Chan-gi Pak and Shun-fat Lung.

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Bibliografiska uppgifter
Materialtyp:	Bok
Språk:	engelska
Ämnen:	Wings (Anatomy) Finite element method. Multidisciplinary design optimization. Tuning. tuning. Finite element method Multidisciplinary design optimization Tuning Flutter analysis. Dynamic structural analysis. Design analysis. Wings. Flight tests. Dynamic models. Ailes (Zoologie) Méthode des éléments finis. Optimisation multidisciplinaire (Conception technique) Accordage.
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