Existence of shocklets in a two-dimensional supersonic mixing layer and its influence on the flow structure.

DOI10.1007/BF02877437zbMath1138.76376MaRDI QIDQ1611730

Heng Zhou, Wei Cao

Publication date: 28 August 2002

Published in: Science in China. Series A (Search for Journal in Brave)

zbMATH Keywords

Tollmien-Schlichting wavedisturbance velocity profileshocklet strength

Mathematics Subject Classification ID

Supersonic flows (76J20)

Related Items (1)

Evolution of a 2-D disturbance in a supersonic boundary layer and the generation of shocklets

Cites Work

• Boundary conditions for direct simulations of compressible viscous flows
• Numerical schemes with high order of accuracy for the computation of shock waves

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