Zobrazeno 1 - 10
of 18
pro vyhledávání: '"Federico Martin de la Escalera"'
Autor:
Yasser Essa, Savvas P. Triantafyllou, Udit Pillai, Federico Martin de la Escalera, Ian Ashcroft
Publikováno v:
Computational Mechanics
We present a phase field based MITC4+ shell element formulation to simulate fracture propagation in thin shell structures. The employed MITC4+ approach renders the element shear- and membrane- locking free, hence providing high-fidelity fracture simu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::653ab097383dd3191cb99996be40c3c1
https://doi.org/10.1007/s00466-020-01827-z
https://doi.org/10.1007/s00466-020-01827-z
Autor:
Federico Martin de la Escalera, Yasser Essa, Jordi Renart, Laura Carreras, Esben Lindgaard, Brian Lau Verndal Bak, Josep Costa, Albert Turon
Publikováno v:
Carreras, L, Renart, J, Turon, A, Costa, J, Bak, B L V, Lindgaard, E, de la Escalera, F M & Essa, Y 2019, ' A benchmark test for validating 3D simulation methods for delamination growth under quasi-static and fatigue loading ', Composite Structures, vol. 210, pp. 932-941 . https://doi.org/10.1016/j.compstruct.2018.12.008
Models for simulating interlaminar crack growth in composites under static and fatigue loads are rarely validated with experimental data different from simple standard tests where the crack front propagates with a uniform shape. The underlying reason
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7f841bdb22670568557df6c55ac23437
https://doi.org/10.1016/j.compstruct.2018.12.008
https://doi.org/10.1016/j.compstruct.2018.12.008
Publikováno v:
Composite Structures
Thin unidirectional-tape and woven-fabric composites are widely utilized in the aerospace and automotive industries due to their enhanced fatigue life and damage resistance. Providing high-fidelity simulations of intra-laminar damage in such laminate
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::24fefb33b673036df23351981cdd7044
Autor:
Josu Etxaniz, Gerardo Aranguren, Sergio Cantero-Chinchilla, Federico Martin de la Escalera, Muhammad Khalid Malik
Publikováno v:
Addi. Archivo Digital para la Docencia y la Investigación
instname
Sensors
Volume 20
Issue 5
Sensors (Basel, Switzerland)
Sensors, Vol 20, Iss 5, p 1445 (2020)
instname
Sensors
Volume 20
Issue 5
Sensors (Basel, Switzerland)
Sensors, Vol 20, Iss 5, p 1445 (2020)
The development of reliable structural health monitoring techniques is enabling a healthy transition from preventive to condition-based maintenance, hence leading to safer and more efficient operation of different industries. Ultrasonic guided-wave b
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d32b5adc1f5cefa051dabd156f0ffae5
http://hdl.handle.net/10810/42451
http://hdl.handle.net/10810/42451
Autor:
Sergio Cantero-Chinchilla, Juan Chiachío, Federico Martin de la Escalera, Dimitrios Chronopoulos, Arthur Jones, Manuel Chiachío, Yasser Essa
Publikováno v:
University of Bristol-PURE
Scopus-Elsevier
Scopus-Elsevier
Bayesian methods for inverse problems offer higher robustness to noise and uncertainty than deterministic, yet accurate, inference methods. Both types of techniques typically focus on finding optimal model parameters that minimize an objective functi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f73f5c29a60cc1e2c5c06bdab71897e9
https://doi.org/10.7712/120119.7121.18810
https://doi.org/10.7712/120119.7121.18810
Autor:
E. Garcia, Yasser Essa, Federico Martin de la Escalera, M. Antonia Sainz Trigo, Pilar Miranzo López, Cinta Marraco-Borderas, Andrés Nistal
Publikováno v:
Boletín de la Sociedad Española de Cerámica y Vidrio, Vol 55, Iss 4, Pp 127-135 (2016)
Marraco-Borderas, C, Nistal, A, García, E, Sainz, M A, Martín De La Escalera, F, Essa, Y & Miranzo, P 2016, ' Análisis de la adhesión de recubrimientos del sistema Y 2 O 3-Al 2 O 3-SiO 2 sobre sustratos de interés para la industria aeroespacial ' Boletin de la Sociedad Espanola de Ceramica y Vidrio, vol. 55, no. 4, pp. 127-135 . DOI: 10.1016/j.bsecv.2016.01.005
Marraco-Borderas, C, Nistal, A, García, E, Sainz, M A, Martín De La Escalera, F, Essa, Y & Miranzo, P 2016, ' Análisis de la adhesión de recubrimientos del sistema Y 2 O 3-Al 2 O 3-SiO 2 sobre sustratos de interés para la industria aeroespacial ' Boletin de la Sociedad Espanola de Ceramica y Vidrio, vol. 55, no. 4, pp. 127-135 . DOI: 10.1016/j.bsecv.2016.01.005
ResumenEn la industria aeroespacial se necesitan materiales ligeros que tengan unas altas prestaciones mecánicas combinadas con una baja densidad. El carburo de silicio, el carbono reforzado con fibra de carbono y el carburo de silicio reforzado con
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d9d48f00a92ebe0660b8a23f9533c5ff
https://doi.org/10.1016/j.bsecv.2016.01.005
https://doi.org/10.1016/j.bsecv.2016.01.005
Autor:
Wouter M. van den Brink, Georgios Kotsinis, Theodoros Loutas, Federico Martin de la Escalera, Panayiotis Tsokanas, Vassilis Kostopoulos
Publikováno v:
Composites Part B: Engineering. 185:107694
The present work presents results from an analysis of the mode I and II interfacial fracture behavior of a new adhesive joint between thin titanium and CFRP adherents, that is destined for application in the future aircraft's leading edge. The joint
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4516d12058ecaecb6e03be5be12cd32a
https://doi.org/10.1016/j.compositesb.2019.107694
https://doi.org/10.1016/j.compositesb.2019.107694
The main challenge of morphing wings is to design a system that is able to withstand the applied loads while being capable of adapting its shape. A multidisciplinary approach is necessary for merging properly with integrated structural actuation syst
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bb05ff8a07d873a6faff41b98f0e7076
https://doi.org/10.1016/b978-0-08-100964-2.00019-8
https://doi.org/10.1016/b978-0-08-100964-2.00019-8
Autor:
Jordi Llobet, Pere Maimi, Albert Turon, Brian Lau Verndal Bak, Esben Lindgaard, Yasser Essa, Federico Martin de la Escalera
Publikováno v:
Llobet, J, Maimi, P, Turon, A, Bak, B L V, Lindgaard, E, Essa, Y & Martin de la Escalera, F 2018, Progressive Damage Modelling of Notched Carbon/Epoxy Laminates Under Tensile Fatigue Loadings . in Progressive Damage Modelling of Notched Carbon/Epoxy Laminates Under Tensile Fatigue Loadings : proceedings of 18th European Conference on Composite Materials (ECCM18) . European Conference on Composite Materials, ECCM, Athen, 18th European Conference on Composite Materials, Athens, Greece, 24/06/2018 .
Scopus-Elsevier
Aalborg University
Scopus-Elsevier
Aalborg University
This work aims to simulate the initiation and propagation of intralaminar and interlaminar damage in open-hole carbon/epoxy laminates subjected to tension-tension fatigue loadings. The model is defined in the framework of damage mechanics and impleme
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::393e505eaaa6ab5f5eda8f0ec05276e3
https://vbn.aau.dk/da/publications/0a93cd05-43fd-405e-abfc-35b4a9806dde
https://vbn.aau.dk/da/publications/0a93cd05-43fd-405e-abfc-35b4a9806dde