Numerical Simulation of Viscous Shock Layer Flows
- Indbinding:
- Paperback
- Sideantal:
- 346
- Udgivet:
- 28. Oktober 2010
- Udgave:
- 11995
- Vægt:
- 577 g.
Leveringstid:
2-3 uger
Forventet levering: 9. Oktober 2024
Beskrivelse af Numerical Simulation of Viscous Shock Layer Flows
The flow field around a body moving at supersonic speed can be divided into three parts, namely, shock layer, near wake including base flow, and far wake. The shock layer flow is bounded by the bow shock wave and the front and lat eral parts of the body surface.
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