Study for Effectiveness of Idealized Theory for Fuselage Section Through Finite Element Analysis

[1]  Richard Degenhardt,et al.  Degradation investigation in a postbuckling composite stiffened fuselage panel , 2008 .

[2]  Vassilis Kostopoulos,et al.  Blast response of metal composite laminate fuselage structures using finite element modelling , 2011 .

[3]  Hamid Zahrouni,et al.  An ABAQUS toolbox for multiscale finite element computation , 2013 .

[4]  J. J. Roseman.  A pointwise estimate for the stress in a cylinder and its application to Saint-Venant's principle , 1966 .

[5]  B. D. Caddock,et al.  Microporous materials with negative Poisson's ratios. II. Mechanisms and interpretation , 1989 .

[6]  Wenhao Wang,et al.  Effects of connective parts on stability of folded stringers stiffened composite panel , 2016 .

[7]  Yalin Yu,et al.  Stress transfer analysis of unidirectional composites with randomly distributed fibers using finite element method , 2015 .

[8]  H. Gerçek,et al.  Poisson's ratio values for rocks , 2007 .

[9]  P. Feraboli,et al.  Four-point bend interlaminar shear testing of uni- and multi-directional carbon/epoxy composite systems , 2003 .

[10]  Francis Collombet,et al.  Numerical and experimental value added of Multi-Instrumented Technological Evaluator for the analysis of thick monolithic composite structures with singularity details , 2015 .

[11]  Richard Degenhardt,et al.  A study on the robustness of two stiffened composite fuselage panels , 2010 .

[12]  Pierre Ladevèze,et al.  Construction of a micromechanics-based intralaminar mesomodel, and illustrations in ABAQUS/Standard , 2008 .

[13]  V. Ho-Huu,et al.  Optimization of laminated composite plates for maximizing buckling load using improved differential evolution and smoothed finite element method , 2016 .

[14]  Yuming Mo,et al.  Experimental and numerical investigation of stiffened composite curved panel under shear and in-plane bending , 2016 .

[15]  M. A. McCarthy,et al.  Finite element analysis of catastrophic failure of dynamically-loaded countersunk composite fuselage joints , 2015 .

[16]  W. Köster,et al.  POISSON'S RATIO FOR METALS AND ALLOYS , 1961 .

[17]  D. Dumas,et al.  From stacking sequences to ply layouts: An algorithm to design manufacturable composite structures , 2016 .