Segueix
Chen Wang(王晨)
Chen Wang(王晨)
College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics (NUAA)
Correu electrònic verificat a nuaa.edu.cn
Títol
Citada per
Citada per
Any
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
752021
Conceptual study of a morphing winglet based on unsymmetrical stiffness
C Wang, HH Khodaparast, MI Friswell
Aerospace Science and Technology 58, 546-558, 2016
292016
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
262020
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
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
252018
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
252018
Smart skin and actuators for morphing structures
J Qiu, C Wang, C Huang, H Ji, Z Xu
Procedia IUTAM 10, 427-441, 2014
252014
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
132020
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
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
112019
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
Compliant structures based on stiffness asymmetry
C Wang, HH Khodaparast, MI Friswell, AD Shaw
The Aeronautical Journal 122 (1249), 442-461, 2018
82018
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
72019
Predicting global strain limits for corrugated panels
C Wang, Y Xia, MI Friswell, EIS Flores
Composite Structures 231, 111472, 2020
62020
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
52022
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
En aquests moments el sistema no pot dur a terme l'operació. Torneu-ho a provar més tard.
Articles 1–20