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Baozhong Sun

Donghua University - Center for Civil Aviation Composites

Shanghai

China

SCHOLARLY PAPERS

8

DOWNLOADS

361

TOTAL CITATIONS

0

Scholarly Papers (8)

1.

Ballistic Penetration Damage of Carbon/Kevlar/Uhmwpe Fiber Hybrid Laminates with Different Hybridization Ratios

Number of pages: 40 Posted: 28 Feb 2023
Zhiyong Li, Yousong Xue, Baozhong Sun and Bohong Gu
Donghua University, Donghua University, Donghua University - Center for Civil Aviation Composites and Donghua University - Center for Civil Aviation Composites
Downloads 169 (454,356)

Abstract:

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Hybrid effect, hybrid ratios, hybrid laminated composite, ballistic impact damage, finite element analysis.

2.

Dynamic Capillary-Driven Additive Manufacturing of Continuous Carbon Fiber Composite

Number of pages: 51 Posted: 05 Jan 2020
University of Delaware - Department of Mechanical Engineering, University of Delaware - Department of Mechanical Engineering, University of Delaware - Department of Mechanical Engineering, University of Delaware - Department of Electrical & Computer Engineering, University of Delaware - Interdisciplinary Science and Engineering Laboratory, Donghua University - Center for Civil Aviation Composites, Donghua University - Center for Civil Aviation Composites, University of Delaware - Department of Mechanical Engineering and University of Delaware - Department of Mechanical Engineering
Downloads 44 (1,133,231)

Abstract:

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Additive manufacturing, capillary-driven 3D printing, continuous fiber composite, free space printing, thermosetting resin

3.

Thermal strain in 3D braided carbon fiber composites experienced from 20°C to -196°C under quasi-static and transient cooling rates

Number of pages: 42 Posted: 10 Nov 2025
Qiannan Li, Baozhong Sun, Bohong Gu and Meiqi Hu
Donghua University, Donghua University - Center for Civil Aviation Composites, Donghua University - Center for Civil Aviation Composites and Donghua University
Downloads 35 (1,263,436)

Abstract:

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3D braided carbon fiber/epoxy composites, thermal strain, coefficient of thermal expansion (CTE), cooling rate

4.

Biodegradable Hydrogel with Excellent Portability, Stability and Anti-Pollution Performance in Solar-Driven Seawater Desalination

Number of pages: 28 Posted: 02 Apr 2024
Dalian Polytechnic University, Dalian Polytechnic University, Dalian Polytechnic University, Dalian Polytechnic University, Dalian Polytechnic University, Donghua University - Center for Civil Aviation Composites and Dalian Polytechnic University
Downloads 35 (1,249,711)

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Solar interfacial evaporation, Hydrogel, Cellulose nanofibers, desalination, Anti-pollution

5.

Failure Analysis and On-Line Damage Monitoring Based on Deep-Learning for Thermo-Oxidative Aged 3d Angle-Interlock Woven Composites Under Tension

Number of pages: 19 Posted: 16 Jan 2025
Yanan Ke, Chaofeng Han, Baozhong Sun and Xianyan Wu
Jiaxing University, Henan University of Technology, Donghua University - Center for Civil Aviation Composites and Jiaxing University
Downloads 25 (1,385,945)

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3D angle-interlock woven composites, thermo-oxidative aging, damage mechanics, deep learning

6.

Study on the mechanism of in-plane fiber deflection defect in the hot diaphragm preforming

Number of pages: 34 Posted: 04 Mar 2026
affiliation not provided to SSRN, affiliation not provided to SSRN, Donghua University, Donghua University - Center for Civil Aviation Composites, affiliation not provided to SSRN, affiliation not provided to SSRN, affiliation not provided to SSRN and affiliation not provided to SSRN
Downloads 22 (1,436,435)

Abstract:

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A, Thermosetting composites B, Hot diaphragm preforming C, Defect D, Fiber deflection

7.

Mode-I Fracture Failure Mechanism of 3-D Braided Composites Under Low-Velocity Wedge-Loaded Impact

Number of pages: 19 Posted: 04 Jun 2024
Juan Fang, Baozhong Sun and Bohong Gu
Donghua University, Donghua University - Center for Civil Aviation Composites and Donghua University - Center for Civil Aviation Composites
Downloads 18 (1,470,786)

Abstract:

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3-D braided composites, Braided structures, Mode-I fracture, Low-velocity impact (LVI), Finite element analysis (FEA)

8.

Damage mechanism and residual tensile strength of CFRP laminates subjected to continuous laser irradiation

Number of pages: 33 Posted: 06 Feb 2026
affiliation not provided to SSRN, affiliation not provided to SSRN, Donghua University, affiliation not provided to SSRN, Donghua University - Center for Civil Aviation Composites, Air Force Engineering University and Donghua University
Downloads 13 (1,534,404)

Abstract:

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Carbon fiber reinforced polymer, Continuous-wave laser irradiation, Laser-Induced Damage, Residual tensile strength, Laser ablation, Heat-affected zone.