Figure 7 - An AMReX-based Compressible Reacting Flow Solver for High-speed Reacting Flows relevant to Hypersonic Propulsion

(a) Mesh refinement used in channel flow simulation (b) cross-sectional view of the instantaneous Mach number.

Reference

An AMReX-based Compressible Reacting Flow Solver for High-speed Reacting Flows relevant to Hypersonic Propulsion - Scientific Figure on ResearchGate. Available from: https://www.researchgate.net/figure/a-Mesh-refinement-used-in-channel-flow-simulation-b-cross-sectional-view-of-the_fig4_386374118 [accessed 21 Jun 2025]

Caption

Figure 7: (a) Mesh refinement used in channel flow simulation (b) cross-sectional view of the instantaneous Mach number.

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<a href="https://www.researchgate.net/figure/a-Mesh-refinement-used-in-channel-flow-simulation-b-cross-sectional-view-of-the_fig4_386374118"><img src="https://www.researchgate.net/publication/386374118/figure/fig4/AS:11431281294569555@1733239608241/a-Mesh-refinement-used-in-channel-flow-simulation-b-cross-sectional-view-of-the.png" alt="(a) Mesh refinement used in channel flow simulation (b) cross-sectional view of the instantaneous Mach number."/></a>