Wave dynamic processes induced by a supersonic projectile discharging from a shock tube

DOI10.1063/1.1566752zbMath1186.76258OpenAlexW2159161928MaRDI QIDQ3556500

Zonglin Jiang

Publication date: 22 April 2010

Published in: Physics of Fluids (Search for Journal in Brave)

Full work available at URL: http://dspace.imech.ac.cn/handle/311007/16657

zbMATH Keywords

supersonic flowjetsflow simulationflow instabilitydetonation wavesshock tubes

Mathematics Subject Classification ID

Fluid mechanics (76-XX)

Related Items (5)

Flow interactions on supersonic projectiles in transitional ballistic regimes ⋮ Wavenumber-extended high-order oscillation control finite volume schemes for multi-dimensional aeroacoustic computations ⋮ Numerical investigations on dynamic process of muzzle flow ⋮ Dynamics of precision-guided projectile launch: fluid-structure interaction ⋮ A numerical study on the generation of impulsive noise by complex flows discharging from a muzzle

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