Starting of an axisymmetric convergent-divergent nozzle in a hypersonic flow

DOI10.1134/S0015462814040164zbMath1301.76043MaRDI QIDQ477244

Yu. V. Tunik, M. A. Zubin

Publication date: 2 December 2014

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

zbMATH Keywords

Euler equationshypersonic flowoblique shockconvergent-divergent nozzleMach diskdiffuseraerodynamic setupsaxisymmetric gas flowsnozzle starting

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Hypersonic flows (76K05)

Related Items (1)

Numerical solution of test problems using a modified Godunov scheme

Cites Work

• Numerical modeling of detonation combustion of hydrogen-air mixtures in a convergent-divergent nozzle
• Nozzle startup in an oncoming flow
• The amplification of weak shock waves in axisymmetric supersonic flow and their reflection from an axis of symmetry

This page was built for publication: Starting of an axisymmetric convergent-divergent nozzle in a hypersonic flow