Enhancement of blowout limit in a Mach 2.92 cavity-based scramjet combustor by a gliding arc discharge
Yifu Tian, Jiajian Zhu, Mingbo Sun, Hongbo Wang, Yuhui Huang, Rong Feng, Bo Yan, Yongchao Sun, Zun Cai
Topics & Concepts
CombustorScramjetCombustionIgnition systemMaterials scienceFuel injectionPremixed flameMach numberNuclear engineeringMechanicsAerospace engineeringChemistryPhysicsEngineeringOrganic chemistryPlasma and Flow Control in AerodynamicsComputational Fluid Dynamics and AerodynamicsCombustion and Detonation Processes