The performance of a scramjet combustor with cavity for Mach numbers 2.25, 2.52 and 2.75 with hydrogen as a fuel
Namrata Bordoloi, Darya Alontseva, Krishna Murari Pandey, Kaushal Kumar Sharma
Topics & Concepts
ScramjetCombustorMach numberSupersonic speedReynolds-averaged Navier–Stokes equationsAerospace engineeringCombustionMechanicsHypersonic speedPhysicsComputational fluid dynamicsEngineeringChemistryOrganic chemistryComputational Fluid Dynamics and AerodynamicsCombustion and flame dynamicsFluid Dynamics and Turbulent Flows