Controlling transonic region formation in the supersonic flow by jet and near-wall energy supply

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Abstract

Numerical modeling based on the Reynolds-averaged Navier - Stokes equations has shown qualitatively the possibility to realize controlled energy release and to obtain a transonic mode with the help of a transverse control air jet, as in modeling based on the Euler equations. The determining role in ignition in the vortex and detachment regions formed near the jets of hydrogen or ethylene and air are played by shock waves.

Original languageEnglish
Title of host publication19th International Conference on the Methods of Aerophysical Research, ICMAR 2018
Editors Fomin
PublisherAmerican Institute of Physics Inc.
Number of pages6
Volume2027
ISBN (Electronic)9780735417472
DOIs
Publication statusPublished - 2 Nov 2018
Event19th International Conference on the Methods of Aerophysical Research, ICMAR 2018 - Akademgorodok, Novosibirsk, Russian Federation
Duration: 13 Aug 201819 Aug 2018

Publication series

NameAIP Conference Proceedings
PublisherAMER INST PHYSICS
Volume2027
ISSN (Print)0094-243X

Conference

Conference19th International Conference on the Methods of Aerophysical Research, ICMAR 2018
CountryRussian Federation
CityAkademgorodok, Novosibirsk
Period13.08.201819.08.2018

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