Numerical study of the oscillations induced by shock/shock interaction in hypersonic double-wedge flows
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Publication:1932308
DOI10.1007/S00193-008-0138-XzbMath1255.76054OpenAlexW2063692768MaRDI QIDQ1932308
R. S. Myong, T. H. Cho, Zonglin Jiang, Zongmin Hu, Chun Wang
Publication date: 17 January 2013
Published in: Shock Waves (Search for Journal in Brave)
Full work available at URL: http://dspace.imech.ac.cn/handle/311007/84803
Shock waves and blast waves in fluid mechanics (76L05) Finite difference methods applied to problems in fluid mechanics (76M20) Hypersonic flows (76K05)
Related Items (5)
Computational confirmation of an abnormal Mach reflection wave configuration ⋮ Geometric criterion for RR↔MR transition in hypersonic double-wedge flows ⋮ Numerical study of the interaction of type IVr around a double-wedge in hypersonic flow ⋮ Reconsideration of inviscid shock interactions and transition phenomena on double-wedge geometries in a \(M_\infty=9\) hypersonic flow ⋮ Multiple-Temperature Gas-Kinetic Scheme for Type IV Shock/Shock Interaction
Cites Work
- Shocked flows induced by supersonic projectiles moving in tubes
- Wave dynamic processes in cellular detonation reflection from wedges
- Shock/shock and shock/boundary layer interactions in an axisymmetric steady laminar flow
- An investigation into the validation of numerical solutions of complex flowfields
- Self-induced oscillations in the shock wave flow pattern formed in a stationary supersonic flow over a double wedge
- Numerical study of inviscid shock interactions on double-wedge geometries
- CRITICAL HYPERSONIC AEROTHERMODYNAMIC PHENOMENA
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