Jian Deng
Current Organizations / Institutes
The organizations/institutes from the scholar's latest article
Research Subjects
Jian Deng has a total of 87 co-authors. Here are the top co-authors by number of shared publications:
- Guangming Zhou
Nanjing University of Aeronautics and Astronautics
13 shared publications - Deng’aN Cai
Nanjing University of Aeronautics and Astronautics
7 shared publications - Xinwei Wang
State Key Laboratory of Mechanics and Control for Aerospace Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
7 shared publications Zengxian Wang
7 shared publicationsDake Wu
AVIC Chengdu Aircraft Design and Research Institute, Chengdu, China
5 shared publicationsQiang Liu
5 shared publications
Latest Publications
- Open Access
- 1 May 2026
- Published by KEAI Publishing in Defence Technology
- Vol. 59, 231-242
Synergistic effects on damage behavior and failure mechanisms of pre-tensioned hybrid laminates subjected to ballistic impacts
- 1 May 2026
- Published by KEAI Publishing in Defence Technology
- Vol. 59, 231-242
Open AccessSynergistic effects on damage behavior and failure mechanisms of pre-tensioned hybrid laminates subjected to ballistic impacts
- 20 April 2026
- Published by Elsevier in Thin-Walled Structures
- Vol. 227
Mechanical behavior and failure mechanisms of all-composite N-core sandwich panels under in-plane compression
- 20 April 2026
- Published by Elsevier in Thin-Walled Structures
- Vol. 227
Mechanical behavior and failure mechanisms of all-composite N-core sandwich panels under in-plane compression
- Open Access
- 23 February 2026
- Published by Elsevier in SSRN Electronic Journal
Enhanced shear performance and failure mechanisms of origami-inspired all-composite sandwich panel
Although corrugated composite sandwich structures offer attractive specific stiffness and strength, along with straightforward manufacturability, their in-plane shear performance remains a critical weakness that limits applications under complex loading. To overcome this limitation, a novel origami-inspired N-type (ON) all-composite corrugated core is envisioned, which integrates the geometric features of V-type and I-type substructures. To predict its equivalent shear modulus and ultimate shear strength, an analytical model based on strain energy equivalence is developed, explicitly accounting for distinct deformation mechanisms under both longitudinal (Y-direction) and transverse (X-direction) shear. Upon synthesizing V-type and I-type substructures via an origami-folding approach, ON all-composite corrugated core sandwich specimens are fabricated in a single curing cycle using a modular mold. Tests are subsequently performed under both shear orientations. Numerical simulations with the method of finite elements (FE) are also carried out. Both the experimental and FE results validate the analytical model predictions and reveal a multifaceted performance enhancement. Compared to the traditional V-type core sandwich construction, the ON structure exhibits a 1.42-fold increase in specific stiffness under Y-direction shear; while its strength is interface-sensitive, the model indicates equivalent potential for strength enhancement. Under X-direction shear, the ON structure demonstrates exceptional damage tolerance, achieving a specific energy absorption 4.33 times greater than that of the V-type core, due mainly to the load-redistributing function of its intact I-type substructures. These findings demonstrate that the proposed ON configuration provides a balanced and superior shear performance, making it a promising candidate for advanced lightweight primary structures subjected to complex loadings.
- 23 February 2026
- Published by Elsevier in SSRN Electronic Journal
Open AccessEnhanced shear performance and failure mechanisms of origami-inspired all-composite sandwich panel
Although corrugated composite sandwich structures offer attractive specific stiffness and strength, along with straightforward manufacturability, their in-plane shear performance remains a critical weakness that limits applications under complex loading. To overcome this limitation, a novel origami-inspired N-type (ON) all-composite corrugated core is envisioned, which integrates the geometric features of V-type and I-type substructures. To predict its equivalent shear modulus and ultimate shear strength, an analytical model based on strain energy equivalence is developed, explicitly accounting for distinct deformation mechanisms under both longitudinal (Y-direction) and transverse (X-direction) shear. Upon synthesizing V-type and I-type substructures via an origami-folding approach, ON all-composite corrugated core sandwich specimens are fabricated in a single curing cycle using a modular mold. Tests are subsequently performed under both shear orientations. Numerical simulations with the method of finite elements (FE) are also carried out. Both the experimental and FE results validate the analytical model predictions and reveal a multifaceted performance enhancement. Compared to the traditional V-type core sandwich construction, the ON structure exhibits a 1.42-fold increase in specific stiffness under Y-direction shear; while its strength is interface-sensitive, the model indicates equivalent potential for strength enhancement. Under X-direction shear, the ON structure demonstrates exceptional damage tolerance, achieving a specific energy absorption 4.33 times greater than that of the V-type core, due mainly to the load-redistributing function of its intact I-type substructures. These findings demonstrate that the proposed ON configuration provides a balanced and superior shear performance, making it a promising candidate for advanced lightweight primary structures subjected to complex loadings.
- 1 January 2026
- Published by Applied Mathematics and Mechanics in 应用数学和力学
- Vol. 47 (6) , 814-824
含内补片复合材料蜂窝夹芯板贴补修理后的结构抗冲击性能
- 1 January 2026
- Published by Applied Mathematics and Mechanics in 应用数学和力学
- Vol. 47 (6) , 814-824
含内补片复合材料蜂窝夹芯板贴补修理后的结构抗冲击性能
- 23 December 2025
- Published by Springer Nature in Applied Composite Materials
- Vol. 33 (1) , 40
On Dynamic Delamination and Fracture Behavior of Ultra-High Molecular Weight Polyethylene Fiber Reinforced Composite Laminates
- 23 December 2025
- Published by Springer Nature in Applied Composite Materials
- Vol. 33 (1) , 40
On Dynamic Delamination and Fracture Behavior of Ultra-High Molecular Weight Polyethylene Fiber Reinforced Composite Laminates
- 27 November 2025
- Published by Elsevier in Composite Structures
- Vol. 377
An origami-inspired N-type core for all-composite sandwich construction: Enhanced mechanical performance and failure mechanisms
- 27 November 2025
- Published by Elsevier in Composite Structures
- Vol. 377
An origami-inspired N-type core for all-composite sandwich construction: Enhanced mechanical performance and failure mechanisms