关注
Gustavo H. C. Silva
Gustavo H. C. Silva
DLR - German Aerospace Center
在 dlr.de 的电子邮件经过验证
标题
引用次数
引用次数
年份
Uncertainty quantification of aeroelastic stability of composite plate wings using lamination parameters
C Scarth, JE Cooper, PM Weaver, GHC Silva
Composite Structures 116, 84-93, 2014
932014
Random field simulation over curved surfaces: Applications to computational structural mechanics
C Scarth, S Adhikari, PH Cabral, GHC Silva, AP do Prado
Computer Methods in Applied Mechanics and Engineering 345, 283-301, 2019
422019
Free vibration analysis of composite plates by higher-order 1D dynamic stiffness elements and experiments
A Pagani, E Carrera, JR Banerjee, PH Cabral, G Caprio, A Prado
Composite Structures 118, 654-663, 2014
352014
Exact and efficient interpolation using finite elements shape functions
GHC Silva, R Le Riche, J Molimard, A Vautrin
European Journal of Computational Mechanics/Revue Européenne de Mécanique …, 2009
322009
Robust and reliability-based aeroelastic design of composite plate wings
C Scarth, PN Sartor, JE Cooper, PM Weaver, GHC Silva
AIAA Journal 55 (10), 3539-3552, 2017
252017
Effect of levels of fidelity on steady aerodynamic and static aeroelastic computations
A Crovato, HS Almeida, G Vio, GH Silva, AP Prado, C Breviglieri, H Guner, ...
Aerospace 7 (4), 42, 2020
202020
A robust and reliability-based aeroelastic tailoring framework for composite aircraft wings
MF Othman, GHC Silva, PH Cabral, AP Prado, A Pirrera, JE Cooper
Composite Structures 208, 101-113, 2019
202019
Tailoring of a composite regional jet wing using the slice and swap method
GHC Silva, AP do Prado, PH Cabral, R De Breuker, JKS Dillinger
Journal of Aircraft 56 (3), 990-1004, 2019
172019
Identification of material properties using FEMU: application to the open hole tensile test
G Silva, R Le Riche, J Molimard, A Vautrin, C Galerne
Applied Mechanics and Materials 7, 73-78, 2007
162007
Reduced-order analysis of aeroelastic systems with freeplay using an augmented modal basis
GHC Silva, GDB Rossetto, G Dimitriadis
Journal of Aircraft 52 (4), 1312-1325, 2015
132015
Lamination parameters for sandwich and hybrid material composites
GHC Silva, Y Meddaikar
AIAA Journal 58 (10), 4604-4611, 2020
102020
Robust aeroelastic design of composite plate wings
C Scarth, PN Sartor, JE Cooper, PM Weaver, GHC Silva
17th AIAA Non-Deterministic Approaches Conference 2015, AIAA 2015-0918, 2015
102015
Identification of material properties using finite elements and full-field measurements with focus on the characterization of deterministic experimental errors
GHC Silva
ENS des Mines de Saint Etienne, 2009
92009
Dipole-dipole energy transfer mechanism to the blue-white-red color-tunable emission presented by CaYAlO4: Tb3+, Eu3+ biocompatibility material obtained by the simple and low …
RV Perrella, MG Manfré, RR Gonçalves, GH Silva, JH Faleiro, ...
Materials Chemistry and Physics 247, 122855, 2020
82020
Global-local structural analysis of composite wings
E Carrera, A Pagani, G Silva
31th Congress of the International Council of the Aeronautical Sciences, 2018
62018
Skin panel optimization of the common research model wing using sandwich composites
YM Meddaikar, JKS Dillinger, GHC Silva, R De Breuker
Journal of Aircraft 59 (2), 386-399, 2022
42022
A full potential static aeroelastic solver for preliminary aircraft design
A Crovato, R Boman, H Güner, G Dimitriadis, V Terrapon, H Almeida, ...
18th International Forum on Aeroelasticity and Structural Dynamics, 2019
42019
Component-wise models for the accurate dynamic and buckling analysis of composite wing structures
E Carrera, A Pagani, PH Cabral, A Prado, G Silva
ASME International Mechanical Engineering Congress and Exposition 50510 …, 2016
42016
Robust aeroelastic design of a composite wing-box
C Scarth, P Sartor, JE Cooper, P Weaver, G Silva
17th AIAA Non-Deterministic Approaches Conference, 0918, 2015
42015
Aeroelastic Tailoring for Enhanced Aerodynamic Wing Performance
E Krupa, J Cooper, A Pirrera, GHC Silva
5th Aircraft Structural Design Conference, 2016
32016
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