Set-up analysis and optimization of cfd simulations for radial turbines

Engineering Applications of Computational Fluid Mechanics (p. 441-460) - 12/2013

• EISSN 1997-003X
• ISSN 1994-2060

• UC3M

Codimension-three bifurcations in a Bénard-Marangoni problem

Physical review E: statistical, nonlinear, and soft matter physics (p. 1-4) - 7/2013

https://doi.org/10.1103/physreve.88.015001 Ver en origen

• EISSN 1550-2376
• ISSN 1539-3755

• UC3M

Development of a segregated compressible flow solver for turbomachinery simulations

Journal of Applied Fluid Mechanics (p. 673-682) - 10/2014

• EISSN 1735-3645
• ISSN 1735-3572

• UC3M

Analysis of bifurcations in a Benard-Marangoni problem: Gravitational effects

INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER (p. 33-41) - 6/2014

https://doi.org/10.1016/j.ijheatmasstransfer.2014.01.061 Ver en origen

• EISSN 1879-2189
• ISSN 0017-9310

• UC3M

Development and validation of a radial variable geometry turbine model for transient pulsating flow applications

ENERGY CONVERSION AND MANAGEMENT (p. 190-203) - 9/2014

https://doi.org/10.1016/j.enconman.2014.05.072 Ver en origen

• EISSN 1879-2227
• ISSN 0196-8904

• UC3M

Analysis of the numerical diffusion in anisotropic mediums: benchmarks for magnetic field aligned meshes in space propulsion simulations

Applied Sciences - 11/2016

https://doi.org/10.3390/app6110354 Ver en origen

• ISSN 2076-3417

• UC3M

Influence of geometrical parameters on the linear stability of a Bénard-Marangoni problem

PHYSICAL REVIEW E (p. 1-7) - 4/2016

https://doi.org/10.1103/physreve.93.043105 Ver en origen

• EISSN 2470-0053
• ISSN 2470-0045

• UC3M

On the onset of instabilities in a Bénard-Marangoni problem in an annular domain with temperature gradient

Thermal Science (p. S585-S596) - 12/2017

https://doi.org/10.2298/tsci160628277h Ver en origen

• ISSN 0354-9836

• UC3M

Axisymmetric plasma plume characterization with 2D and 3D particle codes

PLASMA SOURCES SCIENCE & TECHNOLOGY (p. 1-13) - 10/2018

https://doi.org/10.1088/1361-6595/aae702 Ver en origen

• EISSN 1361-6595
• ISSN 0963-0252

• UC3M

Experimental characterization of a 1 kW Helicon Plasma Thruster

Vacuum (p. 69-73) - 3/2018

https://doi.org/10.1016/j.vacuum.2017.11.036 Ver en origen

• EISSN 1879-2715
• ISSN 0042-207X

• UC3M

Recursive Computation of Complex Frequencies of Vibrating Non-Viscous Damped Systems

The Ninth International Conference on Engineering Computational Technology - 2014

Editor: CIVIL-COMP LTD

https://doi.org/10.4203/ccp.105.35 Ver en origen

• ISBN 978-1-905088-60-7

• UC3M

Benchmarks for Magnetic Field Aligned Meshes in Electromagnetic Plasma Thruster Simulations

34th International Electric Propulsion Conference - 2015

• UC3M

Evaluation of Erosion Reduction Mechanisms in Hall Effect Thrusters

34th International Electric Propulsion Conference - 2015

• UC3M

NOMADS: development of a versatile plasma discharge simulation plarform for electrinc propulsion

Space Propulsion Conference 2016 - 2016

• UC3M

Hybrid Particle Codes for Electric Propulsion

Spacecraft Charging Technology Conference (SCTC-2016) - 2016

• UC3M

Development of physical models of electron cooling in collisionless plasma thruster plumes

22nd SPINE meeting and workshop - 2016

• UC3M

Collisionless electron cooling in unmagnetized plasma thruster plumes

52th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit (p. 2477-2486) - 2016

Editor: American Institute for Aeronautics and Astronautics

• ISBN 9781510833111

• UC3M

Horizonte ISDEFE: Espacio. Análisis del marco institucional y de las principales líneas de desarrollo e investigación actuales en el área Vigilancia y Seguimiento espaciales (SST)

IV Congreso Nacional de I+D en Defensa y Seguridad - 2016

• UC3M

Experimental performances of a 1 kW HPT by means of plasma diagnosis

35th Intern. Electric Propulsion Conf. - 2017

Editor: Electric Rocket Propulsion Society

• UC3M

Optical Emission Spectroscopy diagnostics of heliconplasma thruster operating with Argon

The 35th International Electric Propulsion Conference (IEPC 2017) (p. 1-10) - 2017

• UC3M

Apoyo en la obtención de las características aerodinámicas de un array de placas

Ejecución: 21-08-2013 - 20-09-2013

Tipo: Regional

Financiado por: ATOS SPAIN, S.A.U.

• UC3M

FP7-SPACE-GA-607457 - LEOSWEEP: "Improving Low Earth Orbit Security With Enhanced Electric Propulsion"

Ejecución: 01-11-2013 - 31-12-2016

Tipo: Europeo

Financiado por: EUROPEAN COMMISSION RESEARCH EXECUTIVE AGENCY

• UC3M

Servicios de Asesoramiento en el área de Cálculo mediante Mecánica de Fluidos Computacional (CFD)

Ejecución: 21-04-2014 - 21-04-2019

Tipo: Regional

Financiado por: COMET INGENIERÍA S.L.

• UC3M

ESP2013-41052-P - Propulsión espacial por plasma: simulación y experimentación

Ejecución: 01-01-2014 - 31-12-2016

Tipo: Nacional

Financiado por: MINISTERIO DE ECONOMÍA, COMERCIO Y EMPRESA

• UC3M

Apoyo en la obtención de las características aerodinámicas de un seguidor solar de doble eje a una velocidad de 15 m/s en inclinaciones de 20-30 y 60.

Ejecución: 30-01-2014 - 28-02-2014

Tipo: Regional

Financiado por: ATOS SPAIN, S.A.U.

• UC3M

Realización de ensayos en arrays de paneles solares en túnel de viento.

Ejecución: 10-06-2014 - 09-08-2014

Tipo: Regional

Financiado por: ATOS SPAIN, S.A.U.

• UC3M

10kW Hall-Effect Thruster Optimized for Space Transportation

Ejecución: 17-03-2014 - 31-07-2014

Tipo: Europeo

Financiado por: SNECMA

• UC3M

Orden compra D0215406-OC-001 Rev.0 - Design and Manufacturing of a Langmuir Probe for the use in RF Generated Plasmas

Ejecución: 17-12-2015 - 16-04-2016

Tipo: Regional

Financiado por: SENER, INGENIERIA Y SISTEMAS, S.A.

• UC3M

Video recording during aerial refuelling hose guillotine rig tests

Ejecución: 16-11-2015 - 31-12-2015

Tipo: Regional

Financiado por: AIRBUS DEFENCE AND SPACE S.A.U.

• UC3M

Nº CW240050 / PO FRW 4500586193 - Development of an advanced axisymmetric model of the full plasma discharge in the Helicon Plasma Thruster

Ejecución: 01-12-2016 - 30-09-2019

Tipo: Europeo

Financiado por: AIRBUS DEFENCE AND SPACE SAS

• UC3M

Fluid modeling and simulation of the electron population in Hall Effect Thrusters with complex magnetic topologies.

Fecha de defensa: 18-06-2018

• UC3M

Axisymmetric simulation codes for Hall effect thrusters and plasma plumes

Fecha de defensa: 31-05-2019

• UC3M