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

This work presents a comprehensive framework for the efficient implementation of finite-volume-based reacting flow solvers, specifically tailored for high speed propulsion applications. Using the exascale computing project (ECP) based AMReX framework, a compressible flow solver for handling high-spe...

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Veröffentlicht in:	arXiv.org 2024-12
Hauptverfasser:	Sharma, Shivank, Bielawski, Ral, Gibson, Oliver, Zhang, Shuzhi, Sharma, Vansh, Rauch, Andreas H, Singh, Jagmohan, Abisleiman, Sebastian, Ullman, Michael, Barwey, Shivam, Raman, Venkat
Format:	Artikel
Sprache:	eng
Schlagworte:	Compressible flow Detonation High speed Hypersonic propulsion Numerical methods Reacting flow Solvers Supersonic aircraft Supersonic combustion ramjet engines
Online-Zugang:	Volltext
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