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Detonation combustion of hydrogen in a convergent-divergent nozzle with a central coaxial cylinder

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Publication:482621
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DOI10.1134/S0015462814050160zbMath1302.76209MaRDI QIDQ482621

Yu. V. Tunik

Publication date: 5 January 2015

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


zbMATH Keywords

Euler equationsshock wavesnumerical modelingconvergent-divergent nozzleMach diskdiffuserdetonation combustionnozzle startingcentral bodycombustion stabilizationhydrogen-air mixtureregular interactionsupersonic body


Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Combustion (80A25) Reaction effects in flows (76V05) Supersonic flows (76J20)


Related Items (1)

Numerical solution of test problems using a modified Godunov scheme




Cites Work

  • 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
  • Nozzle startup in an oncoming flow




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