Segui
Xiaoquan Cheng
Xiaoquan Cheng
School of Aeronautical Science And Engineering, BeiHang University
Email verificata su buaa.edu.cn
Titolo
Citata da
Citata da
Anno
An investigation of hygrothermal effects on adhesive materials and double lap shear joints of CFRP composite laminates
S Liu, X Cheng, Q Zhang, J Zhang, J Bao, X Guo
Composites Part B: Engineering 91, 431-440, 2016
1652016
Lightning strike damage on the composite laminates with carbon nanotube films: Protection effect and damage mechanism
J Zhang, X Zhang, X Cheng, Y Hei, L Xing, Z Li
Composites Part B: Engineering 168, 342-352, 2019
782019
Effect of damage on failure mode of multi-bolt composite joints using failure envelope method
X Cheng, S Wang, J Zhang, W Huang, Y Cheng, J Zhang
Composite Structures 160, 8-15, 2017
612017
Effects of stacking sequence and rotation angle of patch on low velocity impact performance of scarf repaired laminates
X Cheng, X Du, J Zhang, J Zhang, X Guo, J Bao
Composites Part B: Engineering 133, 78-85, 2018
542018
Numerical analysis of bearing failure in countersunk composite joints using 3D explicit simulation method
P Liu, X Cheng, S Wang, S Liu, Y Cheng
Composite Structures 138, 30-39, 2016
542016
Tensile properties of a hybrid bonded/bolted joint: Parameter study
X Li, X Cheng, X Guo, S Liu, Z Wang
Composite Structures 245, 112329, 2020
482020
Low-velocity impact performance and effect factor analysis of scarf-repaired composite laminates
X Cheng, J Zhang, J Bao, B Zeng, Y Cheng, R Hu
International Journal of Impact Engineering 111, 85-93, 2018
482018
Total fatigue life prediction for Ti-alloys airframe structure based on durability and damage-tolerant design concept
J Zhang, X Cheng, Z Li
Materials & Design 31 (9), 4329-4335, 2010
442010
Parameters prediction of cohesive zone model for simulating composite/adhesive delamination in hygrothermal environments
X Cheng, Q Zhang, J Zhang, X Guo, Z Niu
Composites Part B: Engineering 166, 710-721, 2019
382019
Effect of stitching on plain and open-hole strength of CFRP laminates
Y Zheng, X Cheng, B Yasir
Chinese Journal of Aeronautics 25 (3), 473-484, 2012
332012
Robust multi-objective wing design optimization via CFD approximation model
Y Liang, X Cheng, Z Li, J Xiang
Engineering Applications of Computational Fluid Mechanics 5 (2), 286-300, 2011
332011
Multi-objective robust airfoil optimization based on non-uniform rational B-spline (NURBS) representation
Y Liang, XQ Cheng, ZN Li, JW Xiang
Science China Technological Sciences 53, 2708-2717, 2010
332010
Investigation of tensile behavior and influence factors of composite-to-metal 2D-scarf bonded joint
Q Zhang, X Cheng, Y Cheng, W Li, R Hu
Engineering Structures 180, 284-294, 2019
312019
Effect of environment conditions on adhesive properties and material selection in composite bonded joints
J Zhang, X Cheng, X Guo, J Bao, W Huang
International Journal of Adhesion and Adhesives 96, 102302, 2020
292020
Experimental and numerical investigation of composite bolted π-joint subjected to bending load
J Fan, X Cheng, S Wang, X Guo, T Zhang
Composites Part B: Engineering 78, 324-330, 2015
242015
Effect of curing condition on bonding quality of scarf-repaired composite laminates
J Zhang, X Cheng, J Zhang, GUO Xin, W Huang
Chinese Journal of Aeronautics 33 (8), 2257-2267, 2020
212020
Failure mechanisms of scarf-repaired composite laminates under tensile load
Y Baig, X Cheng, HJ Hasham, M Abbas, WA Khan
Journal of the Brazilian Society of Mechanical Sciences and Engineering 38 …, 2016
212016
Damage progressive model of compression of composite laminates after low velocity impact
C Xiao-Quan, L Zhang-neng
Applied Mathematics and Mechanics 26, 618-626, 2005
212005
Experimental and numerical investigation of composite box joint under tensile load
Q Zhang, X Cheng, J Zhang, S Wang, Y Cheng, T Zhang
Composites Part B: Engineering 107, 75-83, 2016
202016
Influence of lateral displacement of the grip on single lap composite-to-aluminum bolted joints
SW Wang, XQ Cheng, X Guo, X Li, G Chen
Experimental Mechanics 56, 407-417, 2016
192016
Il sistema al momento non può eseguire l'operazione. Riprova più tardi.
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