Investigation of certain techniques for stabilizing detonationwaves in a supersonic flow
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Publication:1949707
DOI10.1134/S0015462812060129zbMath1262.76106MaRDI QIDQ1949707
Publication date: 15 May 2013
Published in: Fluid Dynamics (Search for Journal in Brave)
Related Items (3)
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 ⋮ Control of detonation combustion in a high-velocity gas mixture flow
Cites Work
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- Stability of detonation combustion with respect to the variation in the hydrogen concentration at the supersonic nozzle inlet
- Stabilization of detonation combustion in a high-velocity flow of a hydrogen-oxygen mixture
- Numerical modeling of detonation combustion of hydrogen-air mixtures in a convergent-divergent nozzle
- Distinctive features of galloping detonation in a supersonic combustible-mixture flow under an inert gas layer
- Viscous detonation in H2‒O2‒Ar using intrinsic low-dimensional manifolds and wavelet adaptive multilevel representation
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