Design of a Mach 2 shape transition nozzle for lab-scale direct-connect supersonic combustor
Bu-Kyeng Sung, Jeong‐Yeol Choi
Topics & Concepts
NozzleMach numberCombustorSupersonic speedMechanicsRotational symmetryDischarge coefficientBoundary layerFlow (mathematics)Jet (fluid)Aerospace engineeringMaterials scienceMechanical engineeringPhysicsEngineeringCombustionChemistryOrganic chemistryComputational Fluid Dynamics and AerodynamicsAerodynamics and Acoustics in Jet FlowsFluid Dynamics and Turbulent Flows