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Casseau, Vincent and Espinoza, Daniel E. R. and Scanlon, Thomas J. and Brown, Richard E. (2016) A two-temperature open-source CFD model for hypersonic reacting flows, part two : multi-dimensional analysis. Aerospace, 3 (4). ISSN 2052-451X
Casseau, Vincent and Palharini, Rodrigo . and Scanlon, Thomas J. and Brown, Richard E. (2016) A two-temperature open-source CFD model for hypersonic reacting flows, part one : zero-dimensional analysis. Aerospace, 3 (4). ISSN 2052-451X
Book Section
Hoste, Jimmy John O.E. and Casseau, Vincent and Fossati, Marco and Taylor, Ian J. and Gollan, Rowan J.; (2017) Numerical modeling and simulation of supersonic flows in propulsion systems by open-source solvers. In: 21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017. American Institute of Aeronautics and Astronautics Inc, AIAA, CHN. ISBN 9781624104633
Casseau, V. and Scanlon, T. J. and John, B. and Emerson, D. R. and Brown, R. E.; Struchtrup, Henning and Ketsdever, Andrew, eds. (2016) Hypersonic simulations using open-source CFD and DSMC solvers. In: Proceedings of the 30th International Symposium on Rarefied Gas Dynamics. AIP Conference Proceedings, 1786 . American Institute of Physics, CAN. ISBN 9780735414488
Espinoza, Daniel and Casseau, Vincent and Scanlon, Thomas and Brown, Richard; Struchtrup, Henning and Ketsdever, Andrew, eds. (2016) An open-source hybrid CFD-DSMC solver for high speed flows. In: Proceedings of the 30th International Symposium on Rarefied Gas Dynamics. AIP Conference Proceedings, 1786 . American Institute of Physics, CAN. ISBN 9780735414488
Conference or Workshop Item
Casseau, Vincent and Scanlon, Thomas J. and Brown, Richard E. (2015) Development of a two-temperature open source CFD model for hypersonic reacting flows. In: 20th International Space Planes and Hypersonic Systems and Technologies Conference, MHYP15, 2015-07-06 - 2015-07-09.
Scanlon, Thomas and Cassineli Palharini, Rodrigo and White, Craig and Espinoza, Daniel and Casseau, Vincent (2015) Simulations of rarefied and continuum hypersonic flow over re-entry objects. In: 8th European Symposium on Aerothermodynamics for Space Vehicles, 2015-03-02 - 2015-03-06.