Publicaciones (37) Publicaciones de Ramón Antonio Otón Martínez

2023

  1. Experimental Evaluation of the Factors That Influence Cylindrical Water Projection Devices against IEDs

    Applied Sciences (Switzerland), Vol. 13, Núm. 2

  2. Numerical performance of a water source transcritical CO2 heat pump with mechanical subcooling

    Applied Thermal Engineering, Vol. 219

2022

  1. Evaluation of the Use of Different Dedicated Mechanical Subcooling (DMS) Strategies in a Water Source Transcritical CO2 Heat Pump for Space Heating Applications

    Clean Technologies, Vol. 4, Núm. 4, pp. 1208-1226

  2. Impact of an internal heat exchanger on a transcritical CO2 heat pump under optimal pressure conditions: Optimal-pressure performance of CO2 heat pump with IHX

    Applied Thermal Engineering, Vol. 215

  3. Libro de actas XI Congreso Ibérico y IX Congreso Iberoamericano de Ciencias y Técnicas del Frío Cytef2022: Avances en Ciencias y Técnicas del Frío - 11. Cartagena, España, 17-19 abril, 2022 dir. congr.

    Universidad Politécnica de Cartagena

  4. Numerical assessment of the use of a dedicated mechanical subcooling system during hot water generation in a water to water transcritical CO2 heat pump

    Libro de actas XI Congreso Ibérico y IX Congreso Iberoamericano de Ciencias y Técnicas del Frío Cytef2022: Avances en Ciencias y Técnicas del Frío - 11. Cartagena, España, 17-19 abril, 2022 (Universidad Politécnica de Cartagena), pp. 19-25

2021

  1. Capabilities and limitations of Large Eddy Simulation with perfectly stirred reactor assumption for engineering applications of unsteady, hydrogen combustion sequences

    Engineering Applications of Computational Fluid Mechanics, Vol. 15, Núm. 1, pp. 1452-1472

  2. Interdisciplinary connections of manufacturing and fluids areas by studying optimized airfoil shapes.

    IX Congreso Internacional Multidisciplinar de Investigación Educativa 1 y 2 de Julio 2021: Libro de actas #CIMIE21

  3. Mathematical modelling of turbulent combustion of two-phase mixtures of gas and solid particles with a Eulerian–Eulerian approach: The case of hydrogen combustion in the presence of graphite particles

    Mathematics, Vol. 9, Núm. 17

  4. Numerical study on the influence of internal heat exchanger in transcritical CO2 heat pumps under optimal pressure conditions

    Journal of Physics: Conference Series

  5. Three-dimensional numerical modeling of internal ballistics for solid propellant combinations

    Mathematics, Vol. 9, Núm. 21

2020

  1. Evaluation of different models for turbulent combustion of hydrogen-air mixtures. Large Eddy Simulation of a LOVA sequence with hydrogen deflagration in ITER Vacuum Vessel

    Fusion Engineering and Design, Vol. 161

  2. Improvement of the performance of a transcritical CO2 cycle by increasing the subcooling

    X Congreso Ibérico y VIII Congreso Iberoamericano de Ciencias y Técnicas del Frío. CYTEF 2020

  3. Rheology of double-base gelled propellants as the basis for extrusion process modelling: influence of normal force on slip layer and flow curves

    International Journal of Material Forming, Vol. 13, Núm. 2, pp. 219-233

2019

  1. An energetic model for detonation of granulated solid propellants

    Energies, Vol. 12, Núm. 23

  2. Validation of a Multi-Dimensional Model for Unsteady Combustion of AP/HTPB Propellants

    Propellants, Explosives, Pyrotechnics, Vol. 44, Núm. 11, pp. 1482-1493

2017

  1. Analysis of several numerical schemes for the characterization of solid propellant combustion

    Proceedings - 30th International Symposium on Ballistics, BALLISTICS 2017

  2. Characterization of transient propellant combustión

    10º Congreso Nacional Ingeniería Termodinámica: Lérida, del 28 al 30 de junio de 2017

  3. Estado del arte y desarrollo de un propulsante LOVA para munición naval de 76 mm / 62.

    V Congreso Nacional de i+d en defensa y seguridad: Toledo, 22, 23 y 24 de noviembre de 2017

  4. On the accuracy of RANS, DES and LES turbulence models for predicting drag reduction with Base Bleed technology

    Aerospace Science and Technology, Vol. 67, pp. 126-140