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Topological Flame Bifurcation, Aerodynamic Flashback Margins, and Multi-Pathway NOx Scaling in a 3D Swirl-Stabilized 100% Pure Hydrogen Aero-Engine Combustor
hypersonic propulsion and hypersonic aerothermodynamics, aerospace engineering not elsewhere classified, computational methods in fluid flow, heat and mass transfer (incl. computational fluid dynamics), multiphysics flows (incl. multiphase and reacting flows), turbulent flows, hydrogen combustion, aero-engine combustor, computational fluid dynamics (cfd) modeling
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