Ignition and combustion characteristics of supersonic combustor under flight Mach number 2.6–3.8
Jianping Li, Kai Wang, Guiqian Jiao, Zilong Liao, Wenyan Song
Topics & Concepts
CombustorKeroseneCombustionIgnition systemMach numberScramjetSupersonic speedHydrogenMaterials scienceChemistryNuclear engineeringMechanicsAerospace engineeringPhysicsEngineeringOrganic chemistryComputational Fluid Dynamics and AerodynamicsRocket and propulsion systems researchCombustion and flame dynamics