Energy absorption capacity of braided frames under bending loads
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[1] Lloyd V. Smith,et al. Strength design with 2-D triaxial braid textile composites , 1996 .
[2] Prasad Potluri,et al. Flexural and torsional behaviour of biaxial and triaxial braided composite structures , 2006 .
[3] Jong Seh Lee,et al. Buckling of orthotropic plates under various inplane loads , 2006 .
[4] Robert K. Goldberg,et al. Finite Element Model for Failure Study of Two-Dimensional Triaxially Braided Composite , 2011 .
[5] M. P. Nemeth,et al. Improved Design Formulae for Buckling of Orthotropic Plates under Combined Loading , 2008 .
[6] P. Potluri,et al. Mechanics of non-orthogonally interlaced textile composites , 2007 .
[7] I. Koch,et al. Experimental Investigation of the Strain Rate Dependent Behaviour of 2D Biaxially and Triaxially Reinforced Braided Composites , 2014, Applied Composite Materials.
[8] JA Schultz,et al. Meso-scale and multicontinuum modeling of a triaxial braided textile composite , 2013 .
[9] Lloyd V. Smith,et al. Comparison of the biaxial strength properties of braided and laminated carbon fiber composites , 1996 .
[10] Matthias Waimer,et al. Investigation of a crash concept for CFRP transport aircraft based on tension absorption , 2014 .
[11] Matthias Waimer,et al. Dynamic testing and modelling of composite fuselage frames and fasteners for aircraft crash simulations , 2013 .
[12] Israel Herszberg,et al. Mechanical performance of 2-D braided carbon/epoxy composites , 1998 .
[13] Karin Birkefeld,et al. Characterization of Biaxial and Triaxial Braids: Fiber Architecture and Mechanical Properties , 2012, Applied Composite Materials.
[14] M. Fouinneteau. Damage and failure modelling of carbon and glass 2D braided composites , 2006 .
[15] Matthias Waimer. Development of a Kinematics Modelfor the Assessment of Global CrashScenarios of a Composite TransportAircraft Fuselage , 2013 .
[16] José G. Pèrez. Energy Absorption and Progressive Failure Response of Composite Fuselage Frames , 1999 .
[17] Ralf Sturm,et al. Failure of CFRP airframe sandwich panels under crash-relevant loading conditions , 2014 .
[18] Matthias Waimer,et al. Contribution to an improved crash design for a composite transport aircraft fuselage—development of a kinematics model and an experimental component test setup , 2013 .