Development of mathematical model and numerical simulation of plasma ignition of flammable mixture with microwave subcritical streamer discharge

P.V. Bulat; K.N. Volkov; A.I. Melnikova; M.E. Renev

doi:10.1016/j.actaastro.2022.09.015

Development of mathematical model and numerical simulation of plasma ignition of flammable mixture with microwave subcritical streamer discharge

P.V. Bulat
, K.N. Volkov
, A.I. Melnikova
, M.E. Renev

Research output: Contribution to journal › Article › peer-review

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Original language	English
Journal	Acta Astronautica
Early online date	13 Sept 2022
DOIs	https://doi.org/10.1016/j.actaastro.2022.09.015
Publication status	E-pub ahead of print - 13 Sept 2022

Bibliographical note

Note: This work was financially supported by the Ministry of Science and Higher Education of Russian Federation during the implementation of the project ‟Creating a leading scientific and technical reserve in the development of advanced technologies for small gas turbine, rocket and combined engines of ultra-light launch vehicles, small spacecraft and unmanned aerial vehicles that provide priority positions for Russian companies in emerging global markets of the future”, No. FZWF-2020-0015.

Keywords

Mechanical, aeronautical and manufacturing engineering

Access to Document

10.1016/j.actaastro.2022.09.015

Volkov-K-52408-AAMAccepted author manuscript, 3.42 MBLicence: CC BY-NC-ND

https://doi.org/10.1016/j.actaastro.2022.09.015

Cite this

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author = "P.V. Bulat and K.N. Volkov and A.I. Melnikova and M.E. Renev",

note = "Note: This work was financially supported by the Ministry of Science and Higher Education of Russian Federation during the implementation of the project ‟Creating a leading scientific and technical reserve in the development of advanced technologies for small gas turbine, rocket and combined engines of ultra-light launch vehicles, small spacecraft and unmanned aerial vehicles that provide priority positions for Russian companies in emerging global markets of the future”, No. FZWF-2020-0015.",

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AU - Volkov, K.N.

AU - Melnikova, A.I.

AU - Renev, M.E.

N1 - Note: This work was financially supported by the Ministry of Science and Higher Education of Russian Federation during the implementation of the project ‟Creating a leading scientific and technical reserve in the development of advanced technologies for small gas turbine, rocket and combined engines of ultra-light launch vehicles, small spacecraft and unmanned aerial vehicles that provide priority positions for Russian companies in emerging global markets of the future”, No. FZWF-2020-0015.

PY - 2022/9/13

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DO - 10.1016/j.actaastro.2022.09.015

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