About choice of working parameters of pressure recovery systems for high power gas flow chemical lasers. Malkov, V., Boreysho, A., Savin, A., Kiselev, I., & Orlov, A. Proceedings of SPIE - The International Society for Optical Engineering, 4184:419-422, 2001. cited By 3
Paper doi abstract bibtex The working parameters of supersonic diffuser (SD) and supersonic ejector (EJ) in pressure recovery system (PRS) of continuous wave chemical lasers (CCL) were discussed. The scheme solution of PRS and the working parameters of system were determined by output parameters of installation. The supersonic diffuser was analyzed in PRS for slowdown of supersonic flow coming out of resonator cavity. The process of slowdown of supersonic flow in a channel required interaction of oblique shocks with the boundary layers. The subsonic laser flow increased along the channel due to turbulence, gradually catching a flow core.
@ARTICLE{Malkov2001419,
author={Malkov, V.M. and Boreysho, A.S. and Savin, A.V. and Kiselev, I.A. and Orlov, A.E.},
title={About choice of working parameters of pressure recovery systems for high power gas flow chemical lasers},
journal={Proceedings of SPIE - The International Society for Optical Engineering},
year={2001},
volume={4184},
pages={419-422},
doi={10.1117/12.413965},
note={cited By 3},
url={https://www.scopus.com/inward/record.uri?eid=2-s2.0-0035044602&doi=10.1117%2f12.413965&partnerID=40&md5=7135fb615d5512c057b4f7cb8428ba7d},
affiliation={Institute of Theoretical and Applied Mechanics, Novosibirsk, Russian Federation; Baltic State Technical University, St. Petersburg, Russian Federation},
abstract={The working parameters of supersonic diffuser (SD) and supersonic ejector (EJ) in pressure recovery system (PRS) of continuous wave chemical lasers (CCL) were discussed. The scheme solution of PRS and the working parameters of system were determined by output parameters of installation. The supersonic diffuser was analyzed in PRS for slowdown of supersonic flow coming out of resonator cavity. The process of slowdown of supersonic flow in a channel required interaction of oblique shocks with the boundary layers. The subsonic laser flow increased along the channel due to turbulence, gradually catching a flow core.},
issn={0277786X},
language={English},
abbrev_source_title={Proc SPIE Int Soc Opt Eng},
document_type={Article},
source={Scopus},
}
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