Nozzle startup in an oncoming flow

DOI10.1134/S0015462811050115zbMath1233.76071MaRDI QIDQ665666

Yu. V. Tunik

Publication date: 5 March 2012

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

zbMATH Keywords

supersonic flowsubsonic flowconvergent-divergent nozzlegas injectionnozzle startup

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) Supersonic flows (76J20)

Related Items (3)

Detonation combustion of hydrogen in a Laval nozzle under rarefied atmosphere conditions ⋮ 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

Cites Work

• 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
• Unnamed Item

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