Zobrazeno 1 - 10
of 17
pro vyhledávání: '"Pierre Omaly"'
Publikováno v:
Advances in Space Research.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f0dbef1ff525532468bc680738a74129
https://doi.org/10.1016/j.asr.2023.01.062
https://doi.org/10.1016/j.asr.2023.01.062
Autor:
Guillaume Grossir, Pierre Omaly, Stéphane Galera, Pierre Van Hauwaert, Martin Spel, Sebastien Paris, Olivier Chazot, Cédric Thiebaut, Julien Annaloro
Publikováno v:
Acta Astronautica. 171:388-402
To predict the debris survivability during an atmospheric re-entry and assess the prospective risk on ground, CNES develops an engineering tool named DEBRISK, based on an object-oriented approach. This approach is currently limited to primitive shape
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bbfe236e1b50f01acd76ec5c0247f9a1
https://doi.org/10.1016/j.actaastro.2020.03.006
https://doi.org/10.1016/j.actaastro.2020.03.006
Autor:
S.M. Drozdov, V. Ledermann, V. Rivola, M. Spel, E. Constant, Pierre Omaly, C. Vasse, Julien Annaloro
Publikováno v:
Journal of Space Safety Engineering. 7:113-124
CNES develops its spacecraft-oriented tool named PAMPERO since 2013. PAMPERO aims to simulate the complete atmospheric reentry of a spacecraft including the fragmentation and ablation processes. One of its objectives is to provide a support to expert
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c6e43d8949d2db925ed1dbb7f00208aa
https://doi.org/10.1016/j.jsse.2020.04.004
https://doi.org/10.1016/j.jsse.2020.04.004
Publikováno v:
Journal of Space Safety Engineering. 4:15-21
This paper is devoted to the comparison between two aerothermodynamics tools, used to predict the survivability of space debris during the re-entries and assess the prospective risk on ground: SCARAB & PAMPERO. Two test-cases have been identified for
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e73c6bff2f1131c7803eefd141e54f9c
https://doi.org/10.1016/j.jsse.2017.02.004
https://doi.org/10.1016/j.jsse.2017.02.004
Publikováno v:
AIAA Scitech 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b59b0d0e2be305b1b1ec11a99053d039
https://doi.org/10.2514/6.2019-0793
https://doi.org/10.2514/6.2019-0793
Autor:
Oleg Bessonov, Daniil A. Andrienko, Sergey T. Surzhikov, Dmitry Yatsukhno, Philippe-Jean Hebert, Julien Annaloro, Pierre Omaly
Publikováno v:
2018 AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0d23e7399e7a9fb1fc4f8bdf614b8444
https://doi.org/10.2514/6.2018-0982
https://doi.org/10.2514/6.2018-0982
Publikováno v:
ISSW 30
ISSW 30, Jul 2015, Tel Aviv, Israel
30th International Symposium on Shock Waves 1
30th International Symposium on Shock Waves 1, 2017, 978-3-319-46211-0
30th International Symposium on Shock Waves 1 ISBN: 9783319462110
ISSW 30, Jul 2015, Tel Aviv, Israel
30th International Symposium on Shock Waves 1
30th International Symposium on Shock Waves 1, 2017, 978-3-319-46211-0
30th International Symposium on Shock Waves 1 ISBN: 9783319462110
The present work is a first step in computing a reactive gas flow behind a shock wave with detailed collision-radiative models. If simulating high-temperature, high-enthalpy, non-equilibrium gas flows in shock layers has been widely done so far with
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ab25625bf135278eb1d7685c231e1369
https://hal.archives-ouvertes.fr/hal-02104877
https://hal.archives-ouvertes.fr/hal-02104877
Publikováno v:
Journal of Thermophysics and Heat Transfer
Journal of Thermophysics and Heat Transfer, American Institute of Aeronautics and Astronautics, 2014, 28 (4), pp.608-622
Journal of Thermophysics and Heat Transfer, American Institute of Aeronautics and Astronautics, 2014, 28 (4), pp.608-622
Nonequilibrium plasma, produced by the propagation of a shock wave in a shock tube or behind a shock front detached from a body entering a planetary atmosphere, requires the development of state-to-state models. The collisional-radiative model for N2
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::90b683f6b79ca36d11bd06aeebc88fbe
https://hal.archives-ouvertes.fr/hal-02023227
https://hal.archives-ouvertes.fr/hal-02023227
Publikováno v:
13th High-Tech Plasma Processes Conference (htpp-2014)
Gleizes, A. and Schein, J. and Teulet, P. 13th High-Tech Plasma Processes Conference (htpp-2014), 550, pp.UNSP 012049, 2014
Gleizes, A. and Schein, J. and Teulet, P. 13th High-Tech Plasma Processes Conference (htpp-2014), 550, pp.UNSP 012049, 2014
WOS:000346661100049; International audience; Three Collisional-Radiative (CR) models are elaborated and tested in typical atmospheric entry conditions. The first CR model (CoRaM-AIR) is dedicated to the Earth atmospheric entry and is based on an elec
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2dda2ad4652b2d9a659f37d06169695e
https://hal.archives-ouvertes.fr/hal-01612382
https://hal.archives-ouvertes.fr/hal-01612382
Publikováno v:
Physics of Plasmas
Physics of Plasmas, American Institute of Physics, 2012, 19 (7), pp.073515. ⟨10.1063/1.4737147⟩
Physics of Plasmas, American Institute of Physics, 2012, 19 (7), pp.073515. ⟨10.1063/1.4737147⟩
The flow field modeling of planetary entry plasmas, laser-induced plasmas, inductively coupled plasmas, arcjets, etc., requires to use Navier-Stokes codes. The kinetic mechanisms implemented in these codes involve global (effective) rate coefficients
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d998aeeb08bd10f5009a87b002914365
https://hal.archives-ouvertes.fr/hal-02017795
https://hal.archives-ouvertes.fr/hal-02017795