Decision for running hypersonic flow -- CFD Online Discussion Forums

August 13, 2023, 07:57	Decision for running hypersonic flow	#1
erkampasha Member İbrahim Join Date: Jun 2017 Posts: 31 Rep Power: 8	Dear users, I would like to conduct aerodynamic analysis of scramjet. Freestream velocity is corresponding to 4.5 mach. The domain just includes internal domain of the engine (inlet, isolator,combustor and nozzle). I wonder that should i enable chemical reaction mechanism for air dissociation?

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