A TESTRIG TO EVALUATE TURBINE PERFORMANCE, OPERATIONAL STRATEGIES UNDER PULSATING INFLOW CONDITIONS
AIAA Propulsion and Energy Forum ; 2019 ; Indianapolis, Ind.
Pressure gain combustion ; 144-153
2019
Conference paper
English
Raketentriebwerk , Erhöhung , Verbrennung , Turbine , Druck
Testrig for Characterization of Turbo-compressor Acoustic Properties
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