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

DOI10.1134/S0015462810020110zbMath1215.76117MaRDI QIDQ545774

Yu. V. Tunik

Publication date: 22 June 2011

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

zbMATH Keywords

supersonic flowshock waveschemical kineticsconvergent-divergent nozzledetonation combustiongas ignitionthrustthermodynamic properties of components

Mathematics Subject Classification ID

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

Related Items (10)

Stability of gas mixture flow with a stabilized detonation wave in a plane channel with a constriction ⋮ Stabilization of detonation combustion of a high-velocity combustible gas mixture flow in a plane channel ⋮ Detonation combustion of hydrogen in a Laval nozzle under rarefied atmosphere conditions ⋮ Stability of detonation combustion with respect to the variation in the hydrogen concentration at the supersonic nozzle inlet ⋮ Investigation of certain techniques for stabilizing detonationwaves in a supersonic flow ⋮ Mathematical modeling of shock-wave processes under gas solid boundary interaction ⋮ Starting of an axisymmetric convergent-divergent nozzle in a hypersonic flow ⋮ Detonation combustion of hydrogen in a convergent-divergent nozzle with a central coaxial cylinder ⋮ Nozzle startup in an oncoming flow ⋮ Control of detonation combustion in a high-velocity gas mixture flow

Cites Work

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

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