Thermoelastic Formulation of Stiffened, Unsymmetric Composite Panels for Finite Element Analysis of High Speed Aircraft

An emerging technology need for capturing 3-D panel thermoelastic response with 2-D planar finite element models (FEMs) is aided with an equivalent plate stiffness and thermal coefficient formulation. The formulation is general and applies to all panel concepts. Included with the formulation is the...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	Collier, Craig S.
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Composite Materials
Online-Zugang:	Volltext bestellen
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