Analysis of turbojet combustion chamber performances based on flow field simplified mathematical model
Author(s) -
Constantin Rotaru
Publication year - 2017
Publication title -
aip conference proceedings
Language(s) - English
Resource type - Conference proceedings
eISSN - 1551-7616
pISSN - 0094-243X
DOI - 10.1063/1.4981987
Subject(s) - combustion chamber , injector , mechanics , turbine , combustion , mechanical engineering , fluent , computational fluid dynamics , materials science , nuclear engineering , aerospace engineering , engineering , chemistry , physics , organic chemistry
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