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Dive into the research topics where Fangfang Sun is active.

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Featured researches published by Fangfang Sun.


Journal of Thermoplastic Composite Materials | 2017

Experimental investigations on the failures of woven textile sandwich panels

Yang Hu; Wanxin Li; Hualin Fan; Fangfang Sun; Jianfeng Ouyang; Zhanxin Qu; Ning Kuang

To reveal the deformation, strength, and failure modes of woven textile sandwich composites (WTSCs), test methods suggested by national standards were referenced and discussed to carry out flatwise and edgewise compression experiments, uniaxial stretching experiments, and three-point bending experiments according to the structural characteristics of WTSC. Strength and failure modes of WTSCs in flatwise compression and uniaxial tension were acquired. Anisotropy and size dependency of strength and failure modes of WTSC panels in edgewise compression were revealed. Strength of weft-compressed panels has few variations when the length is smaller than 60 mm and then decreases obviously when the length is over 60 mm, accompanying with the failure modes turning from crushing, fracture to buckling. Progressive crushing and bending fracture are two observed post-failure modes. Two competing shear failure modes and facesheet failure were observed in three-point bending experiments. Shear strength of the woven core of WTSC was deduced by beam flexure. To acquire facesheet failure mode by long beam flexure, the span should be above 36 times the thickness of the panel.


Acta Mechanica Solida Sinica | 2016

Light-Weight Design of CRH Wind Deflector Panels based on Woven Textile Sandwich Composites

Hualin Fan; Jianfeng Ouyang; Fangfang Sun; Peishi Yu; Ning Kuang; Yang Hu

The woven textile sandwich composite (WTSC) is a promising lightweight composite. In bending, two competing core shearing failure modes reduce the strength; deflection induced by the core shearing deformation reduces the flexural rigidity. To replace a solid composite laminate, the span of WTSC panel must be greater than a critical value, which was deduced on the condition that the load capacity and flexural rigidity of the WTSC panel are equal to those of the composite laminate. Three WTSC panels were tested in bending, so that the failure modes were observed, and the critical spans were determined. Using the alternative design method, the WTSC based wind deflector with reduced weight has been fabricated and mounted on the CRH (China Railway High-speed).


Composite Structures | 2013

Equivalent analysis and failure prediction of quasi-isotropic composite sandwich cylinder with lattice core under uniaxial compression

Fangfang Sun; Hualin Fan; Chuwei Zhou; Daining Fang


Composites Part A-applied Science and Manufacturing | 2013

Compression and bending performances of carbon fiber reinforced lattice-core sandwich composites

Hualin Fan; Lin Yang; Fangfang Sun; Daining Fang


Thin-walled Structures | 2013

Improved manufacturing method and mechanical performances of carbon fiber reinforced lattice-core sandwich cylinder

Liming Chen; Hualin Fan; Fangfang Sun; Long Zhao; Daining Fang


Composites Part A-applied Science and Manufacturing | 2016

A novel carbon fiber reinforced lattice truss sandwich cylinder: Fabrication and experiments

Wanxin Li; Fangfang Sun; Peng Wang; Hualin Fan; Daining Fang


Composites Science and Technology | 2014

Free vibration behaviors of carbon fiber reinforced lattice-core sandwich cylinder

He Zhang; Fangfang Sun; Hualin Fan; Haosen Chen; Liming Chen; Daining Fang


Mechanics of Materials | 2016

Crushing mechanism of hierarchical lattice structure

Fangfang Sun; Changliang Lai; Hualin Fan; Daining Fang


Materials & Design | 2016

In-plane compression behavior and energy absorption of hierarchical triangular lattice structures

Fangfang Sun; Changliang Lai; Hualin Fan


Composites Science and Technology | 2017

Fabrication and testing of composite orthogrid sandwich cylinder

Shu Jiang; Fangfang Sun; Hualin Fan; Daining Fang

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Changliang Lai

Nanjing University of Aeronautics and Astronautics

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Ming Li

Nanjing University of Aeronautics and Astronautics

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Debo Liu

China Academy of Launch Vehicle Technology

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Shu Jiang

Nanjing University of Aeronautics and Astronautics

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Xi Zhang

China Academy of Launch Vehicle Technology

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Peng Wang

Nanjing University of Aeronautics and Astronautics

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Wanxin Li

Nanjing University of Aeronautics and Astronautics

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