Open AccessFlow parameters at the supersonic combustor entrance at tests in quasistationary impulse regime
Author(s) -
S. A. Akinin,
M. A. Goldfeld,
A. V. Starov
Publication year - 2018
Publication title -
aip conference proceedings
Language(s) - English
Resource type - Conference proceedings
eISSN - 1551-7616
pISSN - 0094-243X
DOI - 10.1063/1.5065334
Subject(s) - combustor , mechanics , mach number , nozzle , supersonic speed , boundary layer , airflow , impulse (physics) , supersonic wind tunnel , specific impulse , fluent , materials science , total air temperature , stagnation pressure , computational fluid dynamics , physics , engineering , mechanical engineering , combustion , classical mechanics , chemistry , organic chemistry , thrust
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