Numerical Analysis of the Hydrodynamic Ram Phenomenon in Aircraft Fuel Tanks

AIAA JOURNAL (p. 1621-1630) - 7/2012

https://doi.org/10.2514/1.j051613 View at source

• EISSN 1533-385X
• ISSN 0001-1452

• UC3M

Numerical modelling of partially filled aircraft fuel tanks submitted to Hydrodynamic Ram

Aerospace Science and Technology (p. 19-28) - 2/2012

https://doi.org/10.1016/j.ast.2011.02.003 View at source

• ISSN 1270-9638

• UC3M

On the influence of filling level in CFRP aircraft fuel tank subjected to high velocity impacts

COMPOSITE STRUCTURES (p. 570-577) - 1/2014

Editor: ELSEVIER CUSTOMER SERVICE

https://doi.org/10.1016/j.compstruct.2013.08.036 View at source

• EISSN 1879-1085
• ISSN 0263-8223

• UC3M
• UC3M

Experimental study of CFRP fluid-filled tubes subjected to high-velocity impact

COMPOSITE STRUCTURES (p. 2598-2609) - 9/2011

https://doi.org/10.1016/j.compstruct.2011.04.025 View at source

• EISSN 1879-1085
• ISSN 0263-8223

• UC3M

Numerical analysis of CFRP fluid-filled tubes subjected to high-velocity impact

COMPOSITE STRUCTURES (p. 286-297) - 2/2013

https://doi.org/10.1016/j.compstruct.2012.09.020 View at source

• EISSN 1879-1085
• ISSN 0263-8223

• UC3M

Numerical prediction of delamination in CFRP drilling

COMPOSITE STRUCTURES (p. 677-683) - 2/2014

https://doi.org/10.1016/j.compstruct.2013.10.014 View at source

• EISSN 1879-1085
• ISSN 0263-8223

• UC3M

Numerical study of composite fragment impacts onto rigid target

COMPOSITE STRUCTURES (p. 172-181) - 11/2018

10.1016/j.compstruct.2018.07.002 View at source

• EISSN 1879-1085
• ISSN 0263-8223

• UC3M

Analysis of high velocity impacts of steel cylinders on thin carbon/epoxy woven laminates

COMPOSITE STRUCTURES (p. 623-629) - 1/2013

https://doi.org/10.1016/j.compstruct.2012.08.015 View at source

• EISSN 1879-1085
• ISSN 0263-8223

• UC3M

Experimental study of the impactor mass effect on the low velocity impact of carbon/epoxy woven laminates

COMPOSITE STRUCTURES (p. 774-781) - 12/2015

https://doi.org/10.1016/j.compstruct.2015.08.027 View at source

• EISSN 1879-1085
• ISSN 0263-8223

• UC3M

The influence of laminate stacking sequence on ballistic limit using a combined Experimental/FEM/Artificial Neural Networks (ANN) methodology

COMPOSITE STRUCTURES (p. 299-308) - 1/2018

https://doi.org/10.1016/j.compstruct.2017.03.068 View at source

• EISSN 1879-1085
• ISSN 0263-8223

• UC3M

Multiscale FE Modelling and Design of Composite Laminates Under Impact. In: Comprehensive Composite Materials II

Comprehensive Composite Materials II (p. 219-238) - 8/2017

Editor: ELSEVIER B.V.

https://doi.org/10.1016/b978-0-12-803581-8.10064-5 View at source

• ISBN 9780081005347

• UC3M

Analysis of high-speed impact problems in the aircraft industry. In: Constitutive Relations under Impact Loadings: Experiments, Theoretical and Numerical Aspects

Constitutive Relations under Impact Loadings: Experiments, Theoretical and Numerical Aspects (p. 137-207) - 6/2014

Editor: SPRINGER

https://doi.org/10.1007/978-3-7091-1768-2 View at source

• ISBN 978-3-7091-1767-5

• UC3M

Soft Impact. In: Encyclopedia of Continuum Mechanics

Encyclopedia of Continuum Mechanics (p. 1-15) - 8/2019

Editor: Springer Berlin / Heidelberg

https://doi.org/10.1007/978-3-662-53605-6_209-1 View at source

• ISBN 978-3-662-53605-6

• UC3M

Analysis of Dynamic Loading of Long Fiber Reinforced Composites. In: Fiber-Reinforced Composites

Fiber-Reinforced Composites (p. 497-526) - 10/2012

Editor: NOVA SCIENCE PUBLISHERS INC

• ISBN 978-1-61470-433-1

• UC3M
• UC3M

Impact of soft body materials, an experimental and numerical approach using a Hopkinson tube: application to substitute bird

11th European LS-DYNA Conference 2017 (p. 1-9) - 2017

Editor: DYNAMORE GMBH

• ISBN 9783981621549

• UC3M

Numerical modelling of the Fluid Structure Interaction using ALE and SPH: The Hydrodynamic Ram Phenomenon

11th European LS-DYNA Conference 2017 (p. 1-11) - 2017

Editor: DYNAMORE GMBH

• ISBN 9783981621549

• UC3M

Numerical analysis of high velocity impacts on tape laminates.

17th International Conference on Composite Structures (ICCS17) - 2013

• UC3M

Experimental analysis of high velocity impacts on tape carbon/epoxy laminates

17th International Conference on Composite Structures (ICCS17) - 2013

• UC3M

Modeling high-speed impact on CFRP's with an energy balance equation

19th DYMAT Technical Meeting: Dynamic Mechanical Behaviour of Polymers and Composites (p. 1-8) - 2010

Editor: DYMAT

• UC3M

CFRP Plates Subjected to Sphere Ice

1st International Conference on Mechanics of Nano, Micro and Macro Composite Structures - 2012

• UC3M

Numerical Modeling of High Velocity Impacts on Composite Laminates

1st International Conference on Mechanics of Nano, Micro and Macro Composite Structures - 2012

• UC3M

Statistical and numerical analysis of wear tool geometry in drilling CFRP

20th International Conference on Composite Materials (ICCM20) (p. 1-10) - 2015

• UC3M

Experimental and numerical analysis of ice sphere impacts

7th International Workshop 2013 on Dynamic Behaviour of Materials and its applications in Industrial Processes - 2013

Editor: COPY RED, S.A.

• ISBN 978-84-940615-5-4

• UC3M

Experimental analysis of an attenuation method for hydrodynamic ram effects

7th International Workshop 2013 on Dynamic Behaviour of Materials and its applications in Industrial Processes (p. 451-462) - 10/2013

Editor: COPY RED, S.A.

10.1016/j.matdes.2018.06.020 View at source

• ISBN 978-84-940615-5-4
• EISSN 1873-4197
• ISSN 0264-1275

• UC3M
• UC3M

P017_1537 - Realización de 2 ensayos de impacto de esfera de hielo sobre paneles de titanio microperforado

Period: 18-04-2017 - 17-07-2017

Type of funding: National

Funding entity: CENTRO DE TECNOLOGIAS AERONAUTICAS PARQUE TECN DE

• UC3M

Pedido nº 3L40000188 Versión nº 1 - RENA-100-SS00-FCT-0002- Ensayos dinámicos de caracterización de aceros y uniones soldadas

Period: 28-04-2017 - 01-10-2017

Type of funding: Regional

Funding entity: NAVANTIA, S.A., S.M.E.

• UC3M

Additional Studies of Impact configurations and method validation

Period: 02-12-2013 - 02-06-2014

Type of funding: Regional

Funding entity: AIRBUS OPERATIONS, S.L.

• UC3M

DPI2013-41094-R - Análisis del comportamiento de laminados carbono/epoxi sometidos a impactos de fragmentos de laminados carbono/epoxi

Period: 01-01-2014 - 31-12-2017

Type of funding: National

Funding entity: MINISTERIO DE ASUNTOS ECONOMICOS Y TRANSFORMACION DIGITAL

• UC3M

Comportamiento ante fractura de materiales compuestos de uso estructural aeronáutico

Period: 19-05-2009 - 18-06-2009

Funding entity: AERNNOVA ENGINEERING SOLUTIONS IBERICA, S.A.

• UC3M

Projectiles for ELEMENT project

Period: 17-03-2020 - 17-04-2020

Type of funding: Regional

Funding entity: AIRBUS OPERATIONS, S.L.

• UC3M

Low level ballistic impacts on metallic and composite plates for method validation

Period: 02-12-2013 - 02-06-2014

Type of funding: Regional

Funding entity: AIRBUS OPERATIONS, S.L.

• UC3M

PEDIDO NÚM. A8221464G - Simulation capabilities for Impact predictive models and blade impact damage characterization.

Period: 07-07-2011 - 30-06-2012

Type of funding: Regional

Funding entity: AIRBUS OPERATIONS, S.L.

• UC3M

UC3M-IME-05-026 - CP05-AVANCE EN EL ESTUDIO DE CRITERIOS DE ROTURA EN CONDICIONES DINÁMICAS DE MATERIALES COMPUESTOS DE USO ESTRUCTURAL

Period: 01-01-2006 - 31-01-2007

Funding entity: COMUNIDAD DE MADRID-UC3M

• UC3M

Análisis de tensiones y deformaciones en los receptores solares centrales.

Period: 01-09-2017 - 01-09-2018

Type of funding: National

Funding entity: FUNDACIÓN IBERDROLA ESPAÑA

• UC3M

ANALISIS<br/> DEL COMPORTAMIENTO DE FRAGMENTOS DE CARBONO/EPOXI EN RÉGIMEN DE IMPACTO

Reading date: 06-06-2017

• UC3M

Análisis y modelización del golpe hidrodinamico en tanques integrados de combustible realizados en material compuesto

Reading date: 15-07-2014

• UC3M

Thermal Stress Analysis of Solar Tubular Receivers

Reading date: 10-12-2020

• UC3M