Figure 11 - An AMReX-based Compressible Reacting Flow Solver for High-speed Reacting Flows relevant to Hypersonic Propulsion

$Figure 11: Instantaneous pressure, temperature, and volumetric heat release rate fields along mid-plane of a 3-D stratified detonation case. Grayscale ahead of the wave denotes H 2 mass fraction, where black represents fuel-lean and white represents fuel-rich.$

Instantaneous pressure, temperature, and volumetric heat release rate fields along mid-plane of a 3-D stratified detonation case. Grayscale ahead of the wave denotes H 2 mass fraction, where black represents fuel-lean and white represents fuel-rich.

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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/nstantaneous-pressure-temperature-and-volumetric-heat-release-rate-fields-along_fig5_386374118 [accessed 23 Jun 2025]

Caption

Figure 11: Instantaneous pressure, temperature, and volumetric heat release rate fields along mid-plane of a 3-D stratified detonation case. Grayscale ahead of the wave denotes H 2 mass fraction, where black represents fuel-lean and white represents fuel-rich.

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<a href="https://www.researchgate.net/figure/nstantaneous-pressure-temperature-and-volumetric-heat-release-rate-fields-along_fig5_386374118"><img src="https://www.researchgate.net/publication/386374118/figure/fig5/AS:11431281294569556@1733239608417/nstantaneous-pressure-temperature-and-volumetric-heat-release-rate-fields-along.ppm" alt="Instantaneous pressure, temperature, and volumetric heat release rate fields along mid-plane of a 3-D stratified detonation case. Grayscale ahead of the wave denotes H 2 mass fraction, where black represents fuel-lean and white represents fuel-rich."/></a>