Profesor jornada completa
- rodrigo.cassineli@usm.cl
- Ir a Scopus
Rodrigo Cassineli
Doctorado (PhD) en Ingeniería Mecánica y Aeroespacial, University of Strathclyde, Escocia.
Magíster (MSc) en Ingeniería y Tecnología Espacial, Instituto Nacional de Investigación Espacial, INPE, Brasil.
Físico, Universidade Federal de São Carlos, UFSCar, Brasil.
Áreas de especialización
Mecánica de Fluidos Computacional, Simulación molecular de gases, Aerotermodinámica y aerodinámica de alta velocidad, Transferencia de calor en sistemas aeroespaciales, Aplicación de técnicas CFD y DSMC a problemas industriales.
Publicaciones Seleccionadas
- PALHARINI, R. S. A; VILA, D. A.; RODRIGUES, D. T.; PALHARINI, R. C.; MATTOS, E. V.; PEDRA, G. U., Assessment of extreme rainfall estimates from satellite-based: Regional analysis. Remote Sensing Applications: Society and Environment, v. 23, p. 100603, 2021.
- PALHARINI, R. S. A.; VILA, D. A.; RODRIGUES, D. T.; QUISPE, D. P.; PALHARINI, R. C.; DE SIQUEIRA, R. A.; DE SOUSA AFONSO, J. M., Assessment of the Extreme Precipitation by Satellite Estimates over South America. Remote Sensing, v. 12, p. 2085, 2020.
- PALHARINI, R. C.; SANTOS, W. F. N., The impact of the length-to-depth ratio on aerodynamic surface quantities of a rarefied hypersonic cavity flow. AEROSPACE SCIENCE AND TECHNOLOGY, v. 88, p. 110-125, 2019.
- PALHARINI, R. C.; SCANLON, T. J. ; WHITE, C., Chemically reacting hypersonic flows over 3D cavities: Flowfield structure characterisation. COMPUTERS & FLUIDS, v. 165, p. 173-187, 2018.
- PALHARINI, R. C.; AZEVEDO, J. LUIZ F., Thermochemical Nonequilibrium Computations of a Brazilian Reentry Satellite. JOURNAL OF SPACECRAFT AND ROCKETS, v. 54, p. 1-6, 2017.
- CASSEAU, V. ; PALHARINI, R. C. ; SCANLON, T. J. ; BROWN, R. E., A Two-Temperature Open-Source CFD Model for Hypersonic Reacting Flows, Part One: Zero-Dimensional Analysis. Aerospace, v. 3, p. 34, 2016.
- SCANLON, T. J. ; WHITE, C.; BORG, M. K.; PALHARINI, R. C. ; FARBAR, E.; BOYD, I. D. ; REESE, J. M.; BROWN, R. E., Open-Source Direct Simulation Monte Carlo Chemistry Modeling for Hypersonic Flows. AIAA JOURNAL, v. 53, p. 1670-1680, 2015.
- PALHARINI, R. C.; WHITE, C. ; SCANLON, T. J. ; BROWN, R. E. ; BORG, M. K. ; REESE, J. M., Benchmark numerical simulations of rarefied non-reacting gas flows using an open-source DSMC code. COMPUTERS & FLUIDS, v. 120C, p. 140-157, 2015.
- PALHARINI, R. C.; SCANLON, T. J. ; REESE, J. M., Aerothermodynamic Comparison of Two- and Three-Dimensional Rarefied Hypersonic Cavity Flows. JOURNAL OF SPACECRAFT AND ROCKETS, v. 51, p. 1619-1630, 2014.
Otras publicaciones
- FORTUNATO, M. N.; PEREIRA, R. R. P. P.; PALHARINI, R. C.; FRANCISCO, C. P. F., Thermochemical Nonequilibrium Computations of Apollo Capsule During the Reentry Phase, 26th International Congress of Mechanical Engineering, Brasil, 2021.
- DREVECK, J. A.; PALHARINI, R. C., Hypersonic Rarefied Gas Flow Over Ramp-like Cavity, 26th International Congress of Mechanical Engineering, Brasil, 2021.
- PEREIRA, R. R. P. P.; PALHARINI, R. C.; DAHER, C.; FRANCISCO, C. P. F., Axisymmetric Rarefied Flow Around a Blunted Body: Numerical and Experimental Comparison, 26th International Congress of Mechanical Engineering, Brasil, 2021.
- GAMBA, E. P. ; PALHARINI, R. C. , Validação do Modelo Numérico e Determinação das Condicões do Escoamento para Simulações CFD na Otimização de Aerofólios de Turbinas Eólicas. Brazil Wind Power, 2020, São Paulo, Brasil, 2020.
- GAMBA, E. P. ; PALHARINI, R. C. , Optimization Design Method for Wind Turbine Airfoils Considering Different Angles of Attack Over NACA 0012. 18th Brazilian Congress of Thermal Sciences and Engineering, Online, Brasil, 2020.
- RIOSECO, D. O. ; PALHARINI, R. C., Altitude Effects on Inflatable Aerodynamic Decelerators for CubeSat Reentry and Recovery. 18th Brazilian Congress of Thermal Sciences and Engineering, Online, Brasil, 2020.
- GAMBA, E. P. ; PALHARINI, R. C., Design Method for Wind Turbine Airfoils by Adjoint Optimization Considering Climate Conditions. AIAA Scitech, Online, USA, 2020
- PALHARINI, R. C.; AZEVEDO, J. L. F. ; WHITE, C., DSMC Computations of SARA Reentry Capsule Exposed to Weakly Ionized Gas Flow. AIAA SciTech, San Diego, California, USA, 2019.
- FRANCISCO, C.; PALHARINI, R. C.; PEREIRA, R. R. P. P., Aerothermodynamis for the Molecular Flow Around a CubeSat. II Congresso Aeroespacial Brasileiro, Santa Maria, Brasil, 2019.
- PALHARINI, R. C.; AZEVEDO, J. L. F., Numerical Investigation of Weakly Ionised Gas Effects on the SARA Surface Quantities. 17th Brazilian Congress of Thermal Sciences and Engineering, Águas de Lindóia, Brasil, 2018.
- PEREIRA, R. R. P. P. ; PALHARINI, R. C. ; AZEVEDO, J. L. F. , RANS and DSMC Hypersonic Flows Simulations Over Reentry Capsules. 17th Brazilian Congress of Thermal Sciences and Engineering, Àguas de Lindóia, Brasil, 2018.
- ALHARINI, R. C.; AZEVEDO, J. L. F., The Influence of Gas-surface Interaction on the Brazilian Reentry Satellite at Rarefied Conditions. 16th Brazilian Congress of Thermal Science and Engineering, Vitória, Brasil, 2016.
- PALHARINI, R. C.; AZEVEDO, J. L. F., Assessment of Rarefaction Effects on the SARA Capsule. 30th Rarefied Gas Dynamics Conference, Victoria, Canada, 2016.
- SCANLON, T. J. ; WHITE, C. ; PALHARINI, R. C., Simulation of Satellite Re-entry Using the Direct Simulation Monte Carlo (DSMC) Method. Stardust Final Conference on Asteroids and Space Debris, ESA-ESTEC, Netherlands, 2016.
- PALHARINI, R. C.; WHITE, C. ; AZEVEDO, J. L. F., Aerothermodynamic Characterization of a Microgravity Experiment Platform’s Re-entry Module. International Workshop in Industrial Mathematics, Campinas, Brasil, 2016.
- VIOTTI, D. F. ; PEREIRA, R. R. P. P. ; CASSEAU, V. ; ESPINOZA, D. ; PALHARINI, R. C. ; AZEVEDO, J. L. F. , A Study of Atmosphere Re-entry Flows Through The Comparison of RANS, DSMC And Experimental Data. 16th Brazilian Congress of Thermal Sciences and Engineering, Vitória, Brasil, 2016.
- SCANLON, T. J. ; PALHARINI, R. C. ; WHITE, C. ; ESPINOZA, D. ; CASSEAU, V. Simulations of Rarefied and Continuum Hypersonic Flow Over Reentry Objects. 8th European Symposium on Aerothermodynamics for Space Vehicles, Lisbon, Portugal, 2015.
- PALHARINI, R. C.; AZEVEDO, J. L. F., Thermochemical Nonequilibrium Computations of a Brazilian Reentry Satellite. 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, UK, 2015.
- PALHARINI, R. C.; AZEVEDO, J. L. F., Simulations of Chemically Reactive Gas Flows Around the SARA Capsule: Effects on the Flowfield Structure. In: 23rd ABCM International Congress of Mechanical Engineering, Rio de Janeiro, Brasil, 2015.
- ALHARINI, R. C.; AZEVEDO, J. L. F., Numerical Investigation of Hypersonic Vehicles under Thermochemical Non-Equilibrium Conditions. I Simpósio Regional de Matemática Aplicada, São José do Rio Preto, Brasil, 2015.
- PALHARINI, R. C.; AZEVEDO, J. L. F., Characterization of SARA´s Wake Flow Structure under Thermochemical Nonequilibrium Conditions. 24th Discrete Simulation of Fluid Dynamics, Edinburgh, UK, 2015.
- SCANLON, T. J. ; PALHARINI, R. C. , Direct Simulation Monte Carlo (DSMC) Modelling Using dsmcFoam. 1st Spacecraft Demise Workshop, Toulouse, France, 2014.
- PALHARINI, R. C.; SCANLON, T. J. ; REESE, J. M. , Effects of Angle of Attack on the Behaviour of Imperfections in Thermal Protection Systems of Re-Entry Vehicles. 29TH INTERNATIONAL SYMPOSIUM ON SHOCK WAVES, 2013, Madison, USA, 2013.
- PALHARINI, R. C.; SCANLON, T. J. . Aerothermodynamic Comparison of Two- and Three-dimensional Rarefied Hypersonic Cavity Flow, 43RD AIAA THERMOPHYSICS CONFERENCE, New Orleans, USA, 2012.
- SANTOS, W. F. N.; PALHARINI, R. C., Length-to-Depth Ratio Effects on Flowfield Structure of Low-Density Hypersonic Cavity Flow. 42nd AIAA Thermophysics Conference, Honolulu, Hawaii, 2012.
Proyectos de investigación
- Strengthening Aerospace Engineering in Chile: a Collaboration Between USM, UChile, and INPE. Concurso de Fomento a la Vinculación Internacional para Instituciones de Investigación Regionales (Proyecto ANID Nº FOVI250021), Investigador Principal, 2021-2022.
- Aerothermodynamic Analysis of Inflatable Aerodynamic Decelerators for CubeSats Reentry and Recovery. Fondecyt de Iniciación a Investigación (Proyecto ANID Nº 11190068), Investigador Principal, 2019-2022.
- Aerothermodynamcs of Inflatable Reentry Decelerators, Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES), Investigador Principal, 2017-2019.
- Aerothermodynamic Characterisation of a Microgravity Experiment Platform’s Re-entry Module, Royal Academy of Engineering, Newton Research Collaboration Programme, Co-Investigador, 2016-2016.
- Numerical Investigation of Hypersonic Vehicles under Thermochemical NonEquilibrium Conditions, São Paulo Research Foundation (FAPESP), Investigador Principal, 2015-2016.
- Atmospheric Reentry Modelling Using an Open-source DSMC Code, The Brazilian National Council for Scientific and Technological Development (CNPq), Investigador principal, 2011-2014.
