Optimization of scramjet inlet based on temperature and Mach number of supersonic combustion
Pedro Paulo Batista de Araújo, Marcos Pereira, George Santos Marinho, João Felipe De Araujo Martos, Paulo Toro
Topics & Concepts
ScramjetMach numberSupersonic speedHypersonic speedMechanicsShock (circulatory)Oblique shockShock waveTotal air temperatureAerospace engineeringMaterials scienceCombustionPhysicsCombustorEngineeringChemistryInternal medicineOrganic chemistryMedicineComputational Fluid Dynamics and AerodynamicsGas Dynamics and Kinetic TheoryPlasma and Flow Control in Aerodynamics