Static Aeroelastic Analysis of Flexible Aircraft with Large Deformations

Author(s):  
Libo Wang ◽  
Changchuan Xie ◽  
Chao Yang
2012 ◽  
Vol 55 (10) ◽  
pp. 2700-2711 ◽  
Author(s):  
Chao Yang ◽  
LiBo Wang ◽  
ChangChuan Xie ◽  
Yi Liu

1976 ◽  
Vol 4 (4) ◽  
pp. 219-232 ◽  
Author(s):  
Ö. Pósfalvi

Abstract The effective elastic properties of the cord-rubber composite are deduced from the principle of virtual work. Such a composite must be compliant in the noncord directions and therefore undergo large deformations. The Rivlin-Mooney equation is used to derive the effective Poisson's ratio and Young's modulus of the composite and as a basis for their measurement in uniaxial tension.


AIAA Journal ◽  
2000 ◽  
Vol 38 ◽  
pp. 843-850
Author(s):  
Seong M. Jeon ◽  
In Lee

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