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.
631276.fig.0012a
(a) Shock-capturing solution
631276.fig.0012b
(b) Shock-fitting (bow shock) solution
631276.fig.0012c
(c) Shock-fitting (bow shock and embedded shock) solution