Effect of local equivalent ratio on spark ignition characteristics in a kerosene scramjet combustor at Mach 4 flight condition
Heng Bao, Daoning Yang, Lijun Yang, Zongyang Wang, Chuanjin Jiang
Topics & Concepts
ScramjetCombustorMach numberSPARK (programming language)Ignition systemAerospace engineeringKeroseneAeronauticsMaterials scienceRamjetHypersonic speedCombustionMechanicsNuclear engineeringEnvironmental scienceEngineeringPhysicsComputer scienceThermodynamicsChemistryProgramming languageOrganic chemistryRocket and propulsion systems researchComputational Fluid Dynamics and AerodynamicsCombustion and flame dynamics