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Chen Wang(王晨)
Chen Wang(王晨)
College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics (NUAA)
Verified email at nuaa.edu.cn
Title
Cited by
Cited by
Year
Aeroelastic model and analysis of an active camber morphing wing
J Zhang, AD Shaw, C Wang, H Gu, M Amoozgar, MI Friswell, BKS Woods
Aerospace Science and Technology 111, 106534, 2021
812021
Conceptual study of a morphing winglet based on unsymmetrical stiffness
C Wang, HH Khodaparast, MI Friswell
Aerospace Science and Technology 58, 546-558, 2016
302016
Twist morphing of a composite rotor blade using a novel metamaterial
H Gu, AD Shaw, M Amoozgar, J Zhang, C Wang, MI Friswell
Composite Structures 254, 112855, 2020
282020
Development of a morphing wingtip based on compliant structures
C Wang, H Haddad Khodaparast, MI Friswell, AD Shaw, Y Xia, P Walters
Journal of Intelligent Material Systems and Structures 29 (16), 3293-3304, 2018
272018
Development of a morphing wingtip based on compliant structures
C Wang, H Haddad Khodaparast, MI Friswell, AD Shaw, Y Xia, P Walters
Journal of Intelligent Material Systems and Structures 29 (16), 3293-3304, 2018
272018
Smart skin and actuators for morphing structures
J Qiu, C Wang, C Huang, H Ji, Z Xu
Procedia IUTAM 10, 427-441, 2014
272014
An equivalent model of corrugated panels with axial and bending coupling
C Wang, HH Khodaparast, MI Friswell, AD Shaw
Computers & Structures 183, 61-72, 2017
262017
INVESTIGATING THE BENEFITS OF MORPHING WING TIP DEVICES-A CASE STUDY
C Wang, HH Khodaparast, MI Friswell
International Forum on Aeroelasticity and Structure Dynamics, 2015
132015
Passive energy balancing design for a linear actuated morphing wingtip structure
J Zhang, C Wang, AD Shaw, M Amoozgar, MI Friswell
Aerospace Science and Technology 107, 106279, 2020
122020
Conceptual-level evaluation of a variable stiffness skin for a morphing wing leading edge
C Wang, H Haddad Khodaparast, MI Friswell, A Magrini, R Ponza, ...
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2019
122019
Lag-twist coupling sensitivity and design for a composite blade cross-section with D-spar
MR Amoozgar, AD Shaw, J Zhang, C Wang, MI Friswell
Aerospace Science and Technology 91, 539-547, 2019
92019
Comparison of Constrained Parameterisation Strategies for Aerodynamic Optimisation of Morphing Leading Edge Airfoil
A Magrini, E Benini, R Ponza, C Wang, HH Khodaparast, MI Friswell, ...
Aerospace 6 (3), 31, 2019
82019
Compliant structures based on stiffness asymmetry
C Wang, HH Khodaparast, MI Friswell, AD Shaw
The Aeronautical Journal 122 (1249), 442-461, 2018
82018
Tailored twist morphing achieved using graded bend–twist metamaterials
H Gu, J Taghipour, AD Shaw, M Amoozgar, J Zhang, C Wang, MI Friswell
Composite Structures 300, 116151, 2022
72022
Predicting global strain limits for corrugated panels
C Wang, Y Xia, MI Friswell, EIS Flores
Composite Structures 231, 111472, 2020
62020
Integration of the Spiral Pulley Negative Stiffness Mechanism into the FishBAC Morphing Wing
C Wang, J Zhang, AD Shaw, M Amoozgar, MI Friswell, BKS Woods
9th ECCOMAS Themat. Conf. Smart Struct. Mater.(SMART 2019), Paris, France, 2019
52019
Experimental study of lag-twist coupling concept for rotor blade application
H Gu, M Amoozgar, AD Shaw, J Zhang, C Wang, MI Friswell
Composite Structures 275, 114417, 2021
32021
Design and optimisation of morphing aircraft
C Wang
Swansea University, 2018
22018
Resonant passive energy balancing for a morphing helicopter blade
J Zhang, AD Shaw, C Wang, H Gu, M Amoozgar, MI Friswell
Aerospace Science and Technology 128, 107786, 2022
12022
Experimental validation of inertial twist concept for rotor blade application
H Gu, J Taghipour, A Rivero, M Amoozgar, AD Shaw, J Zhang, C Wang, ...
Composite Structures 288, 115414, 2022
12022
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Articles 1–20