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Modelling and Simulation in Engineering
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Modelling and Simulation in Engineering
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2012
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Article
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Fig 12
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Research Article
The Role of Mesh Generation, Adaptation, and Refinement on the Computation of Flows Featuring Strong Shocks
Figure 12
Supersonic (
𝑀
∞
=
4
.
0
4
) flow past a cylinder with conical flare: pressure isocontours predicted by the shock capturing and shock fitting calculations.
(a)
Shock-capturing solution
(b)
Shock-fitting (bow shock) solution
(c)
Shock-fitting (bow shock and embedded shock) solution