Open AccessThe effect of backpressure on the transition to subsonic flow in the diffuser of a supersonic air intake
Author(s) -
B. I. Gutov,
В. И. Звегинцев,
A. Yu. Melnikov
Publication year - 2017
Publication title -
aip conference proceedings
Language(s) - English
Resource type - Conference proceedings
eISSN - 1551-7616
pISSN - 0094-243X
DOI - 10.1063/1.5007489
Subject(s) - diffuser (optics) , mechanics , bandwidth throttling , choked flow , supersonic speed , static pressure , flow (mathematics) , flow coefficient , materials science , ramjet , backflow , flow separation , adverse pressure gradient , open channel flow , back pressure , stagnation pressure , boundary layer , optics , physics , combustor , combustion , mach number , engineering , thermodynamics , chemistry , inlet , mechanical engineering , light source , organic chemistry , gas compressor
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