Nonlinear Aeroelastic Characteristics of a Laminated Composite Wing Considering Compressible Shock Wave Effects

In this study, advanced computational analysis system for nonlinear static aeroelastic problems has been successfully developed by the composite structure (FEM)-fluid (CFD) combined method with internal iteration steps. Major focus of the present study is to investigate the static aeroelastic charac...

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Veröffentlicht in:	Key engineering materials 2007-03, Vol.334-335, p.481-484
Hauptverfasser:	Lee, Seok Soon, Kim, Dong Hyun, Oh, Il Kwon, Kim, Hyun Jung
Format:	Artikel
Sprache:	eng
Online-Zugang:	Volltext
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