Stabilization of detonation combustion in a high-velocity flow of a hydrogen-oxygen mixture

DOI10.1134/S0015462808060161zbMath1210.76206MaRDI QIDQ532275

Yu. V. Tunik

Publication date: 26 April 2011

Published in: Fluid Dynamics (Search for Journal in Brave)

zbMATH Keywords

chemical kineticsdetonation combustiongas ignitionthrustsupersonic nozzlethermodynamic properties of components

Mathematics Subject Classification ID

Combustion (80A25) Reaction effects in flows (76V05)

Related Items (4)

Investigation of certain techniques for stabilizing detonationwaves in a supersonic flow ⋮ Detonation combustion of hydrogen in a convergent-divergent nozzle with a central coaxial cylinder ⋮ Nozzle startup in an oncoming flow ⋮ Numerical modeling of detonation combustion of hydrogen-air mixtures in a convergent-divergent nozzle

Cites Work

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