DETONATION LIMITS, VELOCITY DEFICITS OF CH4, C2H4, C2H6, C3H8 WITH N2O IN A SMALL DIAMETER TUBE
AIAA Propulsion and Energy Forum ; 2019 ; Indianapolis, Ind.
Pressure gain combustion ; 74-85
2019
Conference paper
English
Raketentriebwerk , Erhöhung , Verbrennung , Turbine , Druck