Research Article

The Role of Mesh Generation, Adaptation, and Refinement on the Computation of Flows Featuring Strong Shocks

Figure 11

Supersonic ( 𝑀 = 4 . 0 4 ) flow past a cylinder with conical flare.
631276.fig.0011a
(a) Shadowgraph, reprinted from [63]
631276.fig.0011b
(b) Fitted shock surfaces