Shocked flows induced by supersonic projectiles moving in tubes

DOI10.1016/S0045-7930(03)00041-0zbMath1100.76547OpenAlexW1997936550MaRDI QIDQ597068

Zonglin Jiang, Kazuyoshi Takayama, Yong-hui Huang

Publication date: 6 August 2004

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/s0045-7930(03)00041-0

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Finite difference methods applied to problems in fluid mechanics (76M20) Supersonic flows (76J20)

Related Items (7)

Numerical simulation of the muzzle flows with base bleed projectile based on dynamic overlapped grids ⋮ Numerical study of the oscillations induced by shock/shock interaction in hypersonic double-wedge flows ⋮ Effect of vent opening area and arrangement on gas flow field as gas propelled cylinder exits a flow tube ⋮ Sharp interface simulations with local mesh refinement for multi-material dynamics in strongly shocked flows ⋮ 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 ⋮ Coupled fluid-solid interaction under shock wave loading

Cites Work

• Flux vector splitting of the inviscid gasdynamic equations with application to finite-difference methods
• An investigation into the validation of numerical solutions of complex flowfields
• Approximate nonreflecting inflow-outflow boundary conditions for the calculation of navier-stokes equations in internal flows

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