Stability of detonation combustion with respect to the variation in the hydrogen concentration at the supersonic nozzle inlet

DOI10.1134/S0015462811010133zbMath1235.76041MaRDI QIDQ408733

Yu. V. Tunik

Publication date: 11 April 2012

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

zbMATH Keywords

supersonic flowchemical kineticsconvergent-divergent nozzledetonation combustiongas ignitiongas mixturesthrust

Mathematics Subject Classification ID

Combustion (80A25) Reaction effects in flows (76V05) Hydrodynamic stability (76E99) Supersonic flows (76J20)

Related Items (3)

Detonation combustion of hydrogen in a Laval nozzle under rarefied atmosphere conditions ⋮ Investigation of certain techniques for stabilizing detonationwaves in a supersonic flow ⋮ Nozzle startup in an oncoming flow

Cites Work

• Numerical modeling of detonation combustion of hydrogen-air mixtures in a convergent-divergent nozzle

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