Zobrazeno 1 - 10
of 65
pro vyhledávání: '"L. Vingert"'
Publikováno v:
Proceedings of the Combustion Institute.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a672128cb923ab8993c7992dc786d6fe
https://doi.org/10.1016/j.proci.2022.07.091
https://doi.org/10.1016/j.proci.2022.07.091
Autor:
R. KAESS, S. KOEGLMEIER, R. BEHR, O. KNAB, D. SAUCEREAU, M. DESENLIS, L. VINGERT, A. NICOLE, T. SCHMITT, S. DUCRUIX, M. THERON, L. LEQUETTE, J. VAN SCHYNDEL, T. HORCHLER, J. HARDI, W. ARMBRUSTER, B. CUENOT, S. BLANCHARD
REST (Rocket Engine Stability initiative) is a European initiative to coordinate and share research activities and to improve the understanding of combustion instability in Liquid Propellant Rocket engines. This is done in different kinds of workshop
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c59f3b0ae3e40611cbd1df4b2dd42dd8
Publikováno v:
Journal of Propulsion and Power. 35:544-551
This work presents the experimental investigation of heat fluxes through the walls of a reduced-scale rocket motor using hydrogen and oxygen as propellants. The engine is water cooled so that it ca...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::85ac28b0f970a79fed8c79063b0386eb
https://doi.org/10.2514/1.b36928
https://doi.org/10.2514/1.b36928
Akademický článek
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Publikováno v:
Acta Astronautica
Acta Astronautica, Elsevier, 2018, pp.1-8. ⟨10.1016/j.actaastro.2018.12.029⟩
Acta Astronautica, Elsevier, 2018, pp.1-8. ⟨10.1016/j.actaastro.2018.12.029⟩
There is a need for experimental data in conditions representative injection in rocket engines to validate or initiate droplet formation models used in numerical simulations. A new cryogenic vessel was built upon the MASCOTTE test bench to study the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::631c25acbc7cd11940d4cd3a715960e5
https://hal.archives-ouvertes.fr/hal-01985725/document
https://hal.archives-ouvertes.fr/hal-01985725/document
Publikováno v:
IFAC-Papers
IFAC-PapersOnLine, Elsevier, 2015, 48 (21), p. 895-900. ⟨10.1016/j.ifacol.2015.09.640⟩
IFAC-PapersOnLine, Elsevier, 2015, 48 (21), p. 895-900. ⟨10.1016/j.ifacol.2015.09.640⟩
International audience; A diagnosis benchmark was developed for the MASCOTTE test bench of ONERA/CNES. It consists of a CARINS Simulator of the bench, model-based fault diagnosis algorithms and firing tests results. The objective of this work was to
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7412ccd1af84de2764cd5c4529af81bb
https://doi.org/10.1016/j.ifacol.2015.09.640
https://doi.org/10.1016/j.ifacol.2015.09.640
Akademický článek
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Publikováno v:
Journal of Propulsion and Power. 14:782-788
In today’ s context of budget cuts and strong competition, reliability, short delays, and cost reduction have become critical issues for combustion device designers, who must seek out new approaches. In this paper, we address the main design issues
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::63fbe1c468a34d4441502ef2c0453c68
https://doi.org/10.2514/2.5341
https://doi.org/10.2514/2.5341
Akademický článek
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Autor:
Frédéric Grisch, P. Grenard, Michael Oschwald, V. I. Fabelinsky, Konstantin A Vereschagin, L. Vingert
Publikováno v:
Progress in Propulsion Physics.
The combustion process in a high-pressure gaseous methane/gaseous oxygen rocket model combustor was investigated by means of optical and laser spectroscopic measurements as well as numerical simulations. Thecombustorwasoperatedatapressureof1.0MPaanda
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9baeb25587b2e49b099b45f0236b6a69
https://doi.org/10.1051/eucass/201304503
https://doi.org/10.1051/eucass/201304503